Administration Federal Aviation 2008 U.S. Commercial Space Transportation Developments and Concepts: Vehicles, Technologies, and Spaceports January 2008 HQ-08368.INDD
AdministrationFederal Aviation
2008 U.S. CommercialSpace TransportationDevelopments and Concepts:Vehicles, Technologies,and Spaceports
January 2008
HQ-08368.INDD
2008 U.S. Commercial Space Transportation Developments and Concepts About FAA/AST
Federal Aviation Administration Office of Commercial Space Transportation i
The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA/AST)
licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of
non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 49 United States
Code, Subtitle IX, Chapter 701 (formerly the Commercial Space Launch Act). FAA/AST’s mission is to
ensure public health and safety and the safety of property while protecting the national security and foreign
policy interests of the United States during commercial launch and reentry operations. In addition, FAA/AST
is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional
information concerning commercial space transportation can be found on FAA/AST’s web site at
http://www.faa.gov/about/office_org/headquarters_offices/ast/.
About the Office of Commercial Space Transportation
About FAA/AST 2008 U.S. Commercial Space Transportation Developments and Concepts
ii Federal Aviation Administration Office of Commercial Space Transportation
NNOOTTIICCEE
Use of trade names or names of manufacturers in this document does not constitute an official endorsement of suchproducts or manufacturers, either expressed or implied, by the Federal Aviation Administration.
Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1
Space Competitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1
Expendable Launch Vehicle Industry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2
Reusable Launch Vehicle Industry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2
Reentry Vehicles and In-Space Technologies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2
Enabling Technologies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3
Spaceports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3
Regulatory Developments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3
Significant 2007 Events . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4
Space Competitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6
Google Lunar X PRIZE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6
X PRIZE Cup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6
America’s Space Prize . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7
Centennial Challenges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7
Expendable Launch Vehicles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9
Current Expendable Launch Vehicle Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9
Atlas V – United Launch Alliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9
Delta II – United Launch Alliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9
Delta IV – United Launch Alliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .10
Minotaur I – Orbital Sciences Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11
Pegasus XL – Orbital Sciences Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11
Taurus – Orbital Sciences Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11
Zenit-3SL – Sea Launch Company, LLC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11
ELV Development Efforts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12
ALV – Alliant Techsystems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12
Aquarius – Space Systems/Loral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12
Eagle S-series – E’Prime Aerospace Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .13
FALCON SLV – Lockheed Martin Michoud Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14
Nanosat Launch Vehicle – Garvey Spacecraft Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14
Sprite SLV – Microcosm, Inc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15
Minotaur IV and V.– Orbital Sciences Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15
QuickReach – AirLaunch LLC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .16
Taurus 2 – Orbital Sciences Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .16
Z-1 – Zig Aerospace, LLC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .16
Zenit-3SLB – Sea Launch Company, LLC, and Space International Services . . . . . . . . . . . . . . .17
NASA Exploration Launch Vehicles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .17
Ares I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .17
Ares V . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18
Sounding Rockets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18
Black Brant – Bristol Aerospace Limited . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18
Oriole – DTI Associates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18
Terrier-Orion – DTI Associates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .19
Hybrid Sounding Rocket Program – Lockheed Martin-Michoud . . . . . . . . . . . . . . . . . . . . . . . . . .19
Hybrid Test Rocket – Lockheed Martin-Michoud and Nammo AS . . . . . . . . . . . . . . . . . . . . . . . .19
SpaceLoft XL – UP Aerospace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20
Reusable Launch Vehicles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .21
Commercial RLV Development Efforts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .21
Tiger & Cardinal – Acuity Technologies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .21
MOD – Armadillo Aerospace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .21
2008 U.S. Commercial Space Transportation Developments and Concepts Contents
Federal Aviation Administration Office of Commercial Space Transportation iii
Table of Contents
BSC Spaceship – Benson Space Company . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .22
New Shepard – Blue Origin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .22
Sea Star – Interorbital Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .23
Neptune – Interorbital Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .23
XA 1.0 – Masten Space Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .24
Crusader LL – Micro-Space . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .24
Crusader HTS – Micro-Space . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .24
Volkon – Paragon Labs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .25
Silver Dart – PlanetSpace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .25
Rocketplane XP – Rocketplane Global . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .25
K-1 – Rocketplane Kistler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .26
SpaceShipTwo – Scaled Composites, LLC/The Spaceship Company/Virgin Galactic . . . . . . . . .27
Dream Chaser – SpaceDev . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .27
Skyhopper – Space Access, LLC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .28
Falcon 1 – Space Exploration Technologies Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .28
Falcon 9 – Space Exploration Technologies Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .29
Laramie Rose – SpeedUp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .29
Michelle-B – TGV Rockets, Inc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .29
Crew Transfer Vehicle – Transformational Space LLC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .30
Burning Splinter – Unreasonable Rocket . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .30
Xerus – XCOR Aerospace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31
Government RLV Development Efforts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31
Space Shuttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31
Fully-Reusable Access to Space Technology Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .32
Reentry Vehicles and In-Space Technology . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .33
Orion Crew Exploration Vehicle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .33
International Space Station Crew and Cargo Transport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .34
SpaceX Dragon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .34
Other Commercial Crew and Cargo Transport Concepts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .35
X-37B Orbital Test Vehicle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .35
Commercial Orbital Habitat Development . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .36
Enabling Technologies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .38
Friction Stir Welding – Space Exploration Technologies Corporation . . . . . . . . . . . . . . . . . . . . . . . . . .38
Composite Tanks – Microcosm, Inc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .38
Solid Engines – Alliant Techsystems, Inc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .38
Liquid Engines – AirLaunch LLC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .39
Liquid Engines – Garvey Spacecraft Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .39
Liquid Engines – Northrop Grumman Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .40
Liquid Engines – Pratt & Whitney Rocketdyne, Inc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .40
Liquid Engines – Space Exploration Technologies Corporation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .41
Liquid Engines – XCOR Aerospace . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .42
Liquid RCS Thruster – Orion Propulsion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .42
Liquid RCS Thruster – Space Exploration Technologies Corporation . . . . . . . . . . . . . . . . . . . . . . . . . .43
Launch Abort System – Orbital Sciences Corporation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .43
Scramjet Propulsion – Pratt & Whitney Rocketdyne . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .43
Propellant Production – Andrews Space . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .44
Air Launch Method – Air Launch LLC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .44
Thermal Protection System – Andrews Space . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .44
Thermal Protection System – Boeing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .45
Stage Recovery System – Alliant Techsystems, Inc. & United Space Alliance LLC . . . . . . . . . . . . . . .45
Contents 2008 U.S. Commercial Space Transportation Developments and Concepts
iv Federal Aviation Administration Office of Commercial Space Transportation
Spaceports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .46
Non-Federal Spaceports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .46
Blue Origin West Texas Launch Site . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .46
California Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .48
Cape Canaveral Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .49
Kodiak Launch Complex . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .50
Mid-Atlantic Regional Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .51
Mojave Air and Space Port . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .53
Oklahoma Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .54
Federal Spaceports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .55
Cape Canaveral Air Force Station . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .55
Edwards Air Force Base . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .55
NASA Kennedy Space Center . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .57
Reagan Test Site . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .57
Vandenberg Air Force Base . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .58
Wallops Flight Facility . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .59
White Sands Missile Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .60
Proposed Non-Federal Spaceports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .60
Cecil Field Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .60
Chugwater Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .62
South Texas Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .63
Spaceport Alabama . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .63
Spaceport America . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .64
Spaceport Sheboygan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .65
Spaceport Washington . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .66
West Texas Spaceport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .66
Regulatory Developments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .68
Private Human Space Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .68
Experimental Launch Permits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .68
Eligibility . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .69
Experimental Permit Compared to a License . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .69
Safety Measures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .69
Operating Area Containment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .70
Key Flight-Safety Event Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .71
Anomaly Reporting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .71
Guidance Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .71
Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .71
Amateur Rocket Classes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .71
What the FAA Proposed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .72
Class 1-Model Rockets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .72
Class 2-Large Model Rockets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .72
Class 3-High-Power Rockets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .72
Class 4-Advanced High-Power Rockets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .73
Information Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .73
Next Steps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .73
Endnotes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .74
Photo Credits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .80
2008 U.S. Commercial Space Transportation Developments and Concepts Contents
Federal Aviation Administration Office of Commercial Space Transportation v
AADC Alaska Aerospace Development
Corporation
ACES Air Collection and Enrichment System
AFB Air Force Base
AGL Above Ground Level
AFRL Air Force Research Laboratory
ALV ATK Launch Vehicle
ARCTUS Advanced Research and Conventional
Technology Utilization Spacecraft
AST Office of Commercial Space
Transportation (within the FAA)
ATK Alliant Techsystems
ATV Automated Transfer Vehicle
AWOS Automated Weather Observing System
BLS Boeing Launch Service
BRAC Base Realignment and Closure
BSC Benson Space Company
CALVEIN California Launch Vehicle Initiative
CCAFS Cape Canaveral Air Force Station
CEV Crew Exploration Vehicle
CONUS Continental United States
COTS Commercial Orbital Transportation
Services
CSIA Clinton-Sherman Industrial Airpark
CSULB California State University, Long Beach
CSLAA Commercial Space Launch
Amendments Act
DARPA Defense Advanced Research Projects
Agency
DoD U.S. Department of Defense
EAFB Edwards Air Force Base
EELV Evolved Expendable Launch Vehicle
ELTR Eastern Launch and Test Range
ELV Expendable Launch Vehicle
ESA European Space Agency
FAA Federal Aviation Administration
FALCON Force Application and Launch from
CONUS
FAST Fully-Reusable Access to Space
Technology
FASTT Freeflight Atmospheric Scramjet Test
Technique
GEM Graphite-Epoxy Motor
GEO Geosynchronous Earth Orbit
GPS/INS Global Positioning System/Inertial
Navigation System
GSC Garvey Spacecraft Corporation
GSLV Geosynchronous Satellite Launch
Vehicle
GTO Geosynchronous Transfer Orbit
HTHL Horizontal Takeoff, Horizontal Landing
HTP High-Test Peroxide
HTPB Hydroxyl Terminated Polybutadiene
HTR Hybrid Test Rocket
HTS Horizontal Test Stand
HX Hydrocarbon X
HYSR Hybrid Sounding Rocket
ICBM Intercontinental Ballistic Missile
IPD Integrated Powerhead Demonstration
IPF Integrated Processing Facility
ISS International Space Station
ISRO Indian Space Research Organization
ITAR International Traffic in Arms
Regulations
Acronyms 2008 U.S. Commercial Space Transportation Developments and Concepts
vi Federal Aviation Administration Office of Commercial Space Transportation
List of Acronyms
JAA Jacksonville Aviation Authority
LAS Launch Abort System
KLC Kodiak Launch Complex
KSC Kennedy Space Center
LAP Launch Assist Platform
LAS Launch Abort System
LASR Large Array of Small Rockets
LC Launch Complex
LEO Low Earth Orbit
LOX Liquid Oxygen
MARS Mid-Atlantic Regional Spaceport
MDA Missile Defense Agency
MEMS Microelectromechanical Systems
MEO Medium Earth Orbit
MRTFB Major Range and Test Facility Base
MSFC Marshall Space Flight Center
MTA Mojave Test Area
NASA National Aeronautics and Space
Administration
NG-LLC Northrop Grumman Lunar Lander
Challenge
NLV Nanosat Launch Vehicle
NPRM Notice of Proposed Rulemaking
NRO National Reconnaissance Office
O/M Oxygen-Methane
ONR Office of Naval Research
ORS Operationally Responsive Spacelift
OSIDA Oklahoma Space Industry Development
Authority
OSP Orbital/Suborbital Program
OTV Orbital Test Vehicle
OV Orbital Vehicle
PDR Preliminary Design Review
PSLV Polar Satellite Launch Vehicle
PWR Pratt & Whitney Rocketdyne
R&D Research and Development
RCS Reaction Control System
RFP Request for Proposals
RLV Reusable Launch Vehicle
RP-1 Rocket Propellant 1
RSRM Reusable Solid Rocket Motor
RSTS Range Safety and Telemetry System
RTS Reagan Test Site
SBIR Small Business Innovation Research
SLC Space Launch Complex
SLF Shuttle Landing Facility
SLV Small Launch Vehicle
SSI Spaceport Systems International
SS/L Space Systems / Loral
SSME Space Shuttle Main Engine
SSO Sun-synchronous Orbit
STEREO Solar Terrestrial Relations
Observatories
STS Space Transportation System
t/LAD Trapeze-Lanyard Air Drop
TBD To Be Determined
TCP/IP Transmission Control Protocol/Internet
Protocol
UAV Unmanned Aerial Vehicle
ULA United Launch Alliance
USAF United States Air Force
VAB Vehicle Assembly Building
2008 U.S. Commercial Space Transportation Developments and Concepts Acronyms
Federal Aviation Administration Office of Commercial Space Transportation vii
VAFB Vandenberg Air Force Base
VaPaK Vapor Pressurization
VTS Vertical Test Stand
VCSFA Virginia Commercial Space Flight
Authority
WAA Wisconsin Aerospace Authority
WIRED Workforce Innovation in Regional
Economic Development
WFF Wallops Flight Facility
WSMR White Sands Missile Range
XA eXtreme Altitude
2008 U.S. Commercial Space Transportation Developments and Concepts
viii Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Introduction
Federal Aviation Administration Office of Commercial Space Transportation 1
2007 was a year of continued steady progress
across the broad spectrum of technology sectors
that together constitute the commercial space indus-
try. Worldwide orbital launches occurred in num-
bers closely mirroring those of the previous two
years, demonstrating that the industry’s recovery
from the sharp downturn in launch activity earlier
in the decade has stabilized. Additionally, develop-
ment and testing of new expendable and reusable
launch vehicles continued, with several vehicles
taking considerable steps toward operability.
The space tourism industry also came into
greater definition in 2007. Virgin Galactic sur-
passed its mark of 100 committed suborbital space-
flight passengers, and had garnered some $31 mil-
lion in revenues from ticket sales as the year
closed. Other companies and private financiers
funded exploration of alternative space tourism
vehicle and spaceport concepts. And in April 2007,
American software developer Charles Simonyi
became the fifth orbital space tourist to visit the
International Space Station (ISS) aboard a Soyuz
flight sponsored by Space Adventures Ltd.
Finally, commercialization initiatives proceed-
ed apace. Following its award of $500 million to
Space Exploration Technologies (SpaceX) and
Rocketplane Kistler (RpK) in 2006 for the agency’s
Commercial Orbital Transportation Services
(COTS) program, NASA in 2007 withdrew the
$174 million remaining in its award to RpK and
began a process of recompeting it among other
vehicle developers. New Mexico again hosted the
X PRIZE Cup, where private vehicle developers
competed a second time for X PRIZE Foundation
and NASA Centennial Challenges awards. And the
United States Department of Defense (DoD), via a
host of initiatives, continued to fund development
of new vehicle families able to launch quickly and
inexpensively, as well as be versatile enough to
serve both military and commercial needs.
This report explores these developments and
other major events that defined U.S. commercial
space transportation in 2007. It showcases current
and planned U.S. commercial or commercially-ori-
ented activities. It also addresses space competi-
tions, reusable launch vehicles (RLVs), expendable
launch vehicles (ELVs), reentry vehicles and in-
space technologies, enabling technologies such as
propulsion and launch configurations, the evolving
array of U.S. spaceports, and new developments in
the regulatory arena.
Whether new developments are highly publi-
cized occurrences or gradual changes, commercial
space transportation remains a dynamic industry.
Providing a broad understanding of today’s com-
mercial launch sector requires examining a wide
range of topics. Information presented in this report
was compiled from open sources and through direct
communication with academic, federal, civil, and
corporate organizations. Because many of the state-
ments herein are forward-looking, the most current
information should be obtained by directly contact-
ing the organizations mentioned in this report.
Space Competitions
In September 2007, a significant new interna-
tional space prize competition was announced
encouraging the private exploration of the Moon.
The Google Lunar X PRIZE was organized by the
X PRIZE Foundation with sponsorship from
Google, along with strategic partnerships with
SpaceX, the SETI Institute, the Saint Louis Science
Center, and the International Space University.
The second X PRIZE Cup took place October
27-28, 2007, at Holloman Air Force Base’s Air and
Space Expo, near Alamogordo, New Mexico. The
Northrop Grumman Lunar Lander Challenge was
held, featuring several rocket flights by Armadillo
Aerospace under an FAA-issued experimental per-
mit. Like the competition held in 2006, none of the
registered participants successfully completed the
challenge criteria. However, promising technologies
were flown and static displays provided interactive
education for the general public.
In 2007, the first prize money was awarded
for the Centennial Challenge program: one prize for
$200,000 was awarded for space technology (astro-
naut gloves). Although participants fell short in
other Centennial Challenges they attempted, several
were determined to try again in 2008, and their
efforts showed promising technological progress.
Introduction
Expendable Launch Vehicle Industry
In 2007, U.S. ELVs—with one notable excep-
tion—maintained launch tempos comparable to the
year prior. The Atlas V, Delta II, Delta IV, Minotaur
I, Pegasus XL, and other ELVs conducted numer-
ous launches, all successful. The Taurus vehicle did
not launch in 2007, but two Taurus launches are
scheduled for 2008. The Sea Launch Zenit-3SL
booster—a major commercial launch provider—
suffered a launch failure in January 2007 that
derailed its use for the remainder of the year.
However, the Zenit-3SL is expected to return to
flight and fully resume its commercial launch
tempo in 2008.
In addition, UP Aerospace conducted the first
successful commercial launch of its SpaceLoft XL
suborbital rocket. The launch was the first success-
ful mission launched from New Mexico’s Spaceport
America.
Several companies continued to develop new
ELV concepts in 2007, including the Alliant
Techsystems (ATK) Launch Vehicle; Aquarius by
Space Systems Loral; Eaglet by E’Prime
Aerospace; Falcon Small Launch Vehicle (SLV) by
Lockheed Martin; Nanosat Launch Vehicle by
Garvey Spacecraft Corporation (GSC); Eagle SLV
by Microcosm; QuickReach by AirLaunch LLC; Z-
1 by Zig Aerospace, LLC; and the Zenit-3SLB
vehicle being developed by Sea Launch. Most of
these designs focus on the small payload market.
Additionally in 2007, NASA further refined
plans for the Ares I and Ares V vehicles, which will
leverage Space Shuttle and Apollo-era technologies
toward future manned and unmanned missions. In
July, NASA awarded Pratt & Whitney Rocketdyne
a $1.2-billion contract to develop the Ares I upper
stage engine, and in August 2007, the agency
selected Boeing to build the Ares I upper stage
itself. Planning for the Ares V was ongoing, with
detailed technical specifications for the vehicle yet
to be announced.
Reusable Launch Vehicle Industry
Several RLV efforts enjoyed notable success-
es in 2007. On the heels of the first FAA-permitted
flight of Blue Origin’s New Shepard rocket in late
2006, the company performed two follow-on test
flights on March 22 and April 19, 2007. Additionally, the
second Falcon 1 launch, designated Demo Flight 2,
took place on March 20, 2007. Although the vehicle
failed to reach orbit because of an upper stage con-
trol anomaly causing the engine to shut down pre-
maturely, SpaceX has taken several steps to resolve
the problem, and a third Falcon 1 flight is expected
in 2008.
Armadillo Aerospace received an experimen-
tal permit for its MOD-1 vehicle in 2007. Under
this permit, on October 20, MOD-1 performed a
low-altitude flight test at the Oklahoma Spaceport
to demonstrate it was capable of performing the
flight profile needed to win Level One of the Lunar
Lander Challenge. MOD-1 then made four flights
at the 2007 X PRIZE Cup in an effort to win the
competition. The vehicle successfully flew the first
leg of the Level One challenge on the afternoon of
October 27, but during the return suffered a “hard
start” of its engine causing a shut down as the vehi-
cle hovered over the landing pad. Despite this
minor setback, Armadillo plans to continue test
flights in 2008.
Other companies pursued ongoing tests of
their respective RLVs in 2007. Among the high-
lights, Masten Space Systems’ XA 0.1 began teth-
ered flight tests, with larger prototype, the XA 0.2,
currently under development; and Rocketplane
Global unveiled a new design for the Rocketplane
XP suborbital vehicle.
Reentry Vehicles and In-SpaceTechnologies
The NASA Vision for Space Exploration,
along with the planned 2010 retirement of the
Space Shuttle, has prompted the need for new reen-
try vehicles and in-space technologies to support
future manned and unmanned missions. To main-
tain mission capability after the Shuttle is retired,
NASA is developing the Orion Crew Exploration
Vehicle to carry people and pressurized cargo into
space. At the end of missions, Orion will also serve
as the atmospheric reentry vehicle. It will reenter
the atmosphere using a newly-developed thermal
protection system. Unmanned abort testing of this
reentry vehicle is slated to begin in 2008.
Among notable other initiatives in this tech-
nology sector, Bigelow Aerospace followed its suc-
Introduction 2008 U.S. Commercial Space Transportation Developments and Concepts
2 Federal Aviation Administration Office of Commercial Space Transportation
cessful 2006 Genesis I mission with a second
orbital habitat demonstration mission, Genesis II, in
2007, as well as preparation of the larger Galaxy
and Sundancer inflatable modules. Galaxy will be a
ground-tested module, though it was originally
planned to be launched into orbit during 2008.
Enabling Technologies
Department of Defense (DoD) needs
remained a primary driver of enabling technology
development in 2007. In July 2007, for example,
DARPA and the USAF jointly agreed to fund Phase
2C of AirLaunch LLC engine tests at a value of
$7.6 million. These Vapor Pressurization (VaPak)
upper stage engines for the AirLaunch QuickReach
Small Launch Vehicle (SLV) would facilitate deliv-
ery of a 450-kilogram (1,000-pound) payload to
low Earth orbit (LEO) for $5 million per launch
with a response time of less than 24 hours—an
application useful to operationally responsive space
and other defense needs.
In addition, a large number of private compa-
nies are developing cryogenic fuel tanks, in-flight
propellant collection systems, advanced liquid-fuel
engines, hybrid rocket motors, more sophisticated
propulsion systems, new launch methodologies
such as air launch, and other technologies and tech-
niques. These enabling technologies can be lever-
aged for a wide variety of defense and other space
access applications.
Spaceports
In 2007, federal and non-federal spaceports
alike sought to expand their capabilities to entice an
emerging responsive and suborbital space tourism
market. These spaceports continued to carry out
launches at similar tempos as in recent years while
implementing infrastructure improvements as fund-
ing allowed and exploring whether and how to
position themselves within the commercial market-
place.
Regulatory Developments
2007 was also a year of ongoing regulatory
enhancements. The FAA continued to refine its reg-
ulations in three primary areas: private human
spaceflight, experimental launches, and amateur
rockets.
2008 U.S. Commercial Space Transportation Developments and Concepts Introduction
Federal Aviation Administration Office of Commercial Space Transportation 3
January 11: China demonstrates a major new mili-
tary space capability by successfully testing an anti-
satellite weapon that destroys the aging Chinese
weather satellite Fengyun 1C. The test creates con-
siderable orbital debris and draws formal protests
from the United States, Australia, Canada, Japan,
South Korea, and other nations.
January 30: A Sea Launch Zenit-3SL rocket
explodes upon liftoff, destroying the vehicle and its
payload, the NSS 8 communications satellite, as
well as damaging the Odyssey Launch Platform.
Russian and Ukrainian authorities identify a foreign
object in an engine turbopump as the likely cause
of the failure.
February 21: NASA Ames Research Center and
space tourism company Virgin Galactic sign a
memorandum of understanding to cooperate on
developing various technologies including space-
suits, thermal protection systems, hybrid propulsion
systems, and hypersonic vehicles.
March 20: Space Exploration Technologies
(SpaceX) conducts the second launch of its Falcon
1 rocket from Kwajalein Atoll in the Pacific Ocean.
The vehicle lifts off successfully and climbs to an
altitude of approximately 300 kilometers (183
miles). However, at five minutes into the flight the
rocket’s second stage experiences a roll control
anomaly and fails to achieve orbit. SpaceX con-
cludes that the anomaly caused propellants to cen-
trifuge away from tank outlets, leading the engine
to shut down prematurely. Although the rocket does
not reach orbit, SpaceX considers the flight a suc-
cess that demonstrated the viability of about 90 per-
cent of the technologies used in the vehicle.
April 3: Voters in New Mexico’s Doña Ana County
approve a sales tax increase designed to raise an
estimated $49 million toward funding Spaceport
America, the future headquarters of Sir Richard
Branson’s Virgin Galactic suborbital space tourism
company.
April 7: The Soyuz ISS 14S mission lifts off from
Baikonur in Kazakhstan carrying the fifth orbital
space tourist to the International Space Station
(ISS). Charles Simonyi, a software architect for-
merly with Microsoft, spends 13 days in space in a
trip organized by the space tourism company Space
Adventures, Ltd. before returning safely to the
Earth on April 21.
April 23: India conducts its first commercial
launch as a Polar Satellite Launch Vehicle (PSLV)
lifts off from Satish Dhawan Space Centre carrying
AGILE, an Italian astrophysics satellite. The launch
is marketed by Antrix, the commercial arm of the
Indian Space Research Organisation (ISRO).
April 28: UP Aerospace conducts the first success-
ful commercial launch of its Spaceloft XL subor-
bital rocket, lofting a Celestis capsule carrying the
cremains of actor James Doohan (the character
“Scotty” from Star Trek), astronaut Gordon Cooper,
and others to an altitude of 115 kilometers (72
miles) before coming down at White Sands Missile
Range. It is the first successful mission launched
from Spaceport America.
May 22: The European Commission and the
European Space Agency (ESA) formally adopt the
first official European Space Policy, a landmark
policy document resulting from nearly three years
of European Space Council meetings involving
consultation with 29 member and observer states. It
expresses that space will play an increasing role in
the security and prosperity of Europe, that
European space assets must be protected from dis-
ruption, and that Europe must maximize its return
on investment in space.
June 7: A Boeing Delta II launches the COSMO-
SkyMed 1 remote sensing satellite from
Vandenberg Air Force Base (VAFB).
July 20: Northrop Grumman Corporation, which
had previously held a 40 percent stake in Scaled
Composites, LLC, announces its acquisition of the
Mojave, California-based developer of the
SpaceShipOne vehicle that captured the Ansari X
Prize in 2004. Both companies state the acquisition
will have no effect on Scaled Composites’ arrange-
ment to provide a fleet of SpaceShipTwo vehicles
to Virgin Galactic.
Significant 2007 Events 2008 U.S. Commercial Space Transportation Developments and Concepts
4 Federal Aviation Administration Office of Commercial Space Transportation
Significant 2007 Events
July 26: A nitrous oxide flash explosion at Mojave
Air and Space Port, California, kills three Scaled
Composites employees and injures three others. The
accident prompts Mojave Air and Space Port and
Scaled Composites officials to review preventive
safety procedures at the launch facility.
September 6: A Proton rocket carrying the
Japanese communications satellite JCSAT 11 does
not reach orbit when the booster’s second stage
fails to separate, causing it to crash in Kazakh terri-
tory downrange from the Baikonur launch site. An
investigation by a Russian State Commission con-
cludes the failure was caused by a defective cable
that prevented the firing of the explosive bolts used
in stage separation. The Proton vehicle returns to
flight on October 26.
September 13: The X PRIZE Foundation and the
Internet search engine company Google unveil the
$30-million Google Lunar X PRIZE competition.
Under the terms of the competition, Google will
award $20 million to the first company to develop a
lunar rover that can soft-land on the Moon, rove at
least 500 meters, and return a series of high-resolu-
tion images and videos. A $5-million prize will be
awarded to the second company to achieve the feat.
The remaining $5 million will fund bonus prizes,
such as discovering lunar water ice. The X PRIZE
Foundation will administer the competition, whose
cash prize expires at the end of 2014.
September 18: A Boeing Delta II launches the
WorldView 1 remote sensing satellite from VAFB.
October 18: NASA terminates an existing agree-
ment with Rocketplane Kistler (RpK) to help fund
development of a reusable launch vehicle after the
30-day notice of termination the agency had given
RpK in September expires. The company was one
of two to win Commercial Orbital Transportation
Services (COTS) demonstration awards. RpK had
taken over the development of the K-1 vehicle orig-
inally proposed by Kistler Aerospace, but had
missed several milestones in its agreement due to
the company's difficulty raising an estimated $500
million from the private sector. NASA announces
plans to hold a competition to award the remaining
money in the RpK award, $174.7 million, with
results to be announced in 2008.
October 27-28: The 2007 X PRIZE Cup is held at
Holloman Air Force Base’s Air and Space Expo in
New Mexico. An estimated 85,000 people over two
days attend this second X PRIZE Cup, an air and
space expo conceived to highlight the emerging
personal spaceflight industry and stage technology
competitions such as the Northrop Grumman Lunar
Lander Challenge.
November 6: Striking machinists involved with
Space Shuttle operations at the Kennedy Space
Center (KSC) reach an agreement with their
employer, United Space Alliance, on a new three-
year contract providing workers with a substantial
portion of the wage increases they had sought and
more limited concessions on benefits.
November 22: Russia announces plans for a new
spaceport, the Vostochny (“Eastern”) cosmodrome,
in the Amur region located in the Far East of the
country. The precise location of the spaceport will
be decided by 2010, with unmanned launches slated
to begin from there by 2015, followed by manned
missions in 2018.
November 24: European Union (EU) member
nations reach an agreement on funding the Galileo
satellite navigation system after deciding to divide
development of the constellation into six contracts
and prohibit any one company from winning more
than two of them. The proposal will fund Galileo at
€2.4 billion (US$3.5 billion) using unspent agricul-
tural subsidies.
December 6: Odyssey Moon, a newly established
international lunar enterprise based in the Isle of
Man, announces it will seek the $30-million Google
Lunar X PRIZE, making the company the first team
to complete registration for entry into the competi-
tion.
December 8: A Boeing Delta II launches the
Cosmo-Skymed 2 remote sensing satellite from
VAFB.
2008 U.S. Commercial Space Transportation Developments and Concepts Significant 2007 Events
Federal Aviation Administration Office of Commercial Space Transportation 5
The U.S. space community has a number of prize
competitions that promote the development of com-
mercial spaceflight technology. Various technolo-
gies and services are being competed in order to
increase the capability of private spacefaring enti-
ties to access and operate within suborbital space,
orbital space, and beyond. These competitions aim
to create commercial space launch services (and
other space capabilities) with lower costs, better
quality, and more efficient processes than the
options currently available. The four sets of current-
ly active prize competitions are the Google Lunar X
PRIZE, the X PRIZE Cup, America’s Space Prize,
and NASA’s various Centennial Challenges.
Google Lunar X PRIZE
In September 2007, the X PRIZE Foundation
announced a new international space prize competi-
tion to encourage the private exploration of the
Moon. The Google Lunar X PRIZE calls for pri-
vately funded teams to land a robot on the surface
of the Moon, explore the surface by traveling at
least 500 meters, and return two packages of high-
resolution video and imagery (called “Mooncasts”)
back to the Earth. The first place winner will claim
$20 million if the prize is won by the end of 2012,
or $15 million if the prize is won in 2013 or 2014.
A second place prize valued at $5 million is avail-
able for the second team to complete the contest
criteria before the end of 2014; it may also be
awarded in place of the first place prize if the first
team partially completes the mission. Additional
bonus prizes worth a total of $5 million will be
available for successfully completing certain com-
plex lunar exploration tasks, bringing the total
Google Lunar X PRIZE purse to $30 million.1
The contest will require teams to use a private
launch, thereby pushing forward commercial launch
vehicle capability and potentially increasing launch
demand.
X PRIZE Cup
The X PRIZE Cup is an annual event to
advance new concepts and technologies that enable
commercial human spaceflight by providing awards
and cash prizes. A secondary priority for the com-
petition is to promote education and awareness in
the general population about advancements in
spaceflight technology. The public has the opportu-
nity to view competitions between providers of
commercial space technology and interact with
aerospace industry pioneers who are working to
reduce the cost and increase the safety and viability
of commercial human space travel. Thus far, two
Cups have been held, plus the “Countdown to the X
PRIZE Cup” in 2005. At both Cups, $2 million in
prizes have been offered as part of the Northrop
Grumman Lunar Lander Challenge, a prize compe-
tition funded by NASA’s Centennial Challenges
program. The eventual goal of the event is to have
teams compete in several categories of human
spaceflight to win the overall X PRIZE Cup, as
well as hold other individual competitions and
Rocket Racing League events. Conceptual Cup cat-
egories include: fastest turnaround time between a
vehicle’s first launch and second landing, maximum
number of passengers per launch, total number of
passengers during the competition, maximum alti-
tude, and fastest flight time. Current vehicle devel-
opment timelines will not allow for these types of
competitions for several years, though other signifi-
cant activities have taken place at the annual event.
The second X PRIZE Cup took place October
27-28, 2007, at Holloman Air Force Base’s Air and
Space Expo, near Alamogordo, New Mexico. The
Northrop Grumman Lunar Lander Challenge (see
the Centennial Challenges section) was held, which
featured several rocket flights by Armadillo
Aerospace under an FAA-issued experimental per-
mit. Like the competition held in 2006, none of the
Space Competitions 2008 U.S. Commercial Space Transportation Developments and Concepts
6 Federal Aviation Administration Office of Commercial Space Transportation
Space Prize Competitions
Lunar rover mockup at the introduction of the Google Lunar X PRIZE
registered participants successfully completed the
challenge criteria, but promising technologies were
flown and static displays provided interactive edu-
cation for the general public.3
America’s Space Prize
Bigelow Aerospace has proposed a commer-
cial spaceflight competition, America’s Space Prize,
to develop affordable spacecraft that could service
their future space complexes. This prize challenges
entities to design a spacecraft without government
funding that is capable of carrying passengers into
orbit with the eventual goal of transporting humans
to Bigelow Aerospace’s expandable space habitats.
According to the rules, competitors will be required
to build a spacecraft capable of carrying a five-per-
son crew to an altitude of 400 kilometers (240
miles) and completing two orbits of the Earth at
that altitude. They must then repeat that accom-
plishment within 60 days. Both flights must carry
passengers, and the second flight must carry a crew
of at least five. The spacecraft will have to dock
with a Bigelow Aerospace space complex or, at a
minimum, demonstrate relevant docking capability.
In addition, no more than 20 percent of the space-
craft can consist of expendable hardware. With the
successful launch and ongoing operation of the
Genesis I and Genesis II pathfinder spacecraft, as
well as the company’s current plans for future hab-
itable complexes, Bigelow Aerospace is aggressive-
ly continuing to build demand for the transportation
systems outlined in the America’s Space Prize com-
petition. The competition deadline is January 10,
2010, with a cash prize of $50 million, funded fully
by Bigelow Aerospace.4
Centennial Challenges
NASA’s Innovative Partnerships Program
(IPP) uses Centennial Challenges to advance the
development of space technologies through prize
competitions, bringing important government
encouragement to commercial efforts. Centennial
Challenges was previously located within the
Exploration Systems Mission Directorate, but was
moved to IPP at the beginning of fiscal year 2007.
This program creates specialized competitions to
stimulate progress on specific technologies related
to exploring space and other NASA missions.
NASA uses funding outlets beyond the standard
procurement process and collaborates with non-
profit organizations to sponsor, promote, and oper-
ate the competitions. There are seven Centennial
Challenges currently active, six of which support
space technology. All of these are open for competi-
tion between U.S. non-governmental entities. Not
all of the competitions deal directly with commer-
cial space transportation technologies, but they do
spur technology development for use in future
space missions, and can drive the demand for
spaceflight. The first award of Centennial
Challenges prize money was made in 2007 for
space technology. Other Centennial Challenge
attempts, while not winning prize money, have
shown promising technological progress.5
The NASA prize competition that correlates
most directly with rocket-powered commercial
space transportation is the Northrop Grumman
Lunar Lander Challenge (NG-LLC). This competi-
tion is administered and executed by the X PRIZE
Foundation, who received funding to cover admin-
istrative costs from Northrop Grumman in
exchange for naming rights of the competition. The
rules of the NG-LLC call for a rocket-propelled
vehicle with an assigned payload mass to demon-
strate its ability to takeoff vertically, fly for a mini-
mum amount of time during which it must reach a
certain altitude, travel
horizontally to a desig-
nated landing area, land
vertically at the landing
area, and complete a
similar return trip within
a set timeframe. The
flight characteristics are
tested at two different
difficulty levels that
have separate prizes
based on increasingly
difficult requirements.
During the 2007 NG-
LLC held at the X
PRIZE Cup, Armadillo
Aerospace was the only
participant to fly a lunar
lander concept, though nine teams had originally
registered to compete.6 Armadillo made four flight
attempts to win the first-level competition using its
MOD-1 vehicle. The team was unable to win the
prize money and did not make an attempt at the
higher-level difficulty requirements, but the team,
2008 U.S. Commercial Space Transportation Developments and Concepts Space Competitions
Federal Aviation Administration Office of Commercial Space Transportation 7
Flight of ArmadilloAerospace’s MOD-1 vehicle for the 2007Northrop Grumman
Lunar Lander Challenge
as in 2006, showed its technological progress
through flight attempts. The total prize money,
$500,000 for level one and $1,500,000 for level
two, will transfer to 2008 when the challenge will
be held again.
The other space-focused Centennial
Challenges, not including the Personal Air Vehicle
Challenge administered and executed by the
Comparative Aircraft Flight Efficiency Foundation,
promote future space mission technologies that
could increase the likelihood for spaceflight and
possibly commercial space transportation. The
Astronaut Glove Challenge (run by Volanz
Aerospace/Spaceflight America) was won in 2007
by Peter Homer for his glove’s best rating in
strength, flexibility, and comfort categories.7 The
contest paid $200,000 and will continue in 2008
with a total of $400,000 in prize money. The first
two Centennial Challenges ever held, and which
will continue in 2008, are the Tether and Beam
Power Challenges (conducted by the Spaceward
Foundation) encouraging the development of high
strength-to-weight materials and wireless power
distribution technologies. The 2007 competitions
were held at the Space Elevator Games on October
19-21 near Salt Lake City, Utah.8 There has yet to
be a winner of these two challenges, so the prize
money will continue to accumulate, increasing in
2008 to $900,000 for each competition. The
Regolith Excavation Challenge, conducted in 2007
with four teams but no winner, and Moon Regolith
Oxygen Extraction Challenge (both run by the
California Space Education and Workforce
Institute) are also active. These Challenges have
prizes amounting to $750,000 and $1 million,
respectively, for future lunar exploration excavation
and oxygen extraction technologies.9 Together, all
these competitions are meeting NASA’s goals of
promoting and publicizing private space technology
development through the investment of non-govern-
mental resources, ingenuity, and innovation.
The President’s Fiscal Year (FY) 2008 Budget
Request asks for $4 million per year for Centennial
Challenges for FY 2008 through FY 2012 as a part
of the IPP.10 The FY 2008 omnibus budget bill
passed by Congress in December 2007 provides no
new funding for Centennial Challenges.11 Despite
the fact that the program’s budget was zeroed out in
FY 2007 by the continuing resolution and in FY
2008 by the omnibus budget bill, the extant compe-
titions are fully-funded and the prize purses are
becoming significantly larger. The funding exists
because NASA has not experienced large associated
program costs to present, which is a result of
administrative and operational cost-shifting through
collaborations with non-profit organizations, and
because unearned prize money has rolled over from
one year to the next. Provided additional appropria-
tions are agreed upon, NASA plans to expand the
number of Centennial Challenges, with more com-
petitions dealing with space exploration, science,
and transportation.
Space Competitions 2008 U.S. Commercial Space Transportation Developments and Concepts
8 Federal Aviation Administration Office of Commercial Space Transportation
This survey of U.S. ELVs is divided into four sec-
tions. The first reviews the ELVs currently avail-
able to serve a wide range of commercial and gov-
ernment payloads. The second reviews a number of
proposed commercial ELVs under study or devel-
opment. Many of these are designed to launch
small satellites at lower costs and quicker than
existing vehicles. The third discusses the new
launch vehicles being developed exclusively to sup-
port the U.S. Vision for Space Exploration. The
final section reviews suborbital sounding rockets
manufactured and operated by U.S. companies.
Current Expendable Launch VehicleSystems
Table 1, on the next page, lists the ELV sys-
tems available in the United States today for com-
mercial, government, or both, missions. The
Minotaur is restricted to government payloads, and
Boeing is currently marketing the Delta IV only to
government customers. Atlas V, Delta II, Pegasus,
and Taurus vehicles are available for commercial
and U.S. government launches; the Zenit-3SL is not
available for U.S. government missions.
Atlas V – United Launch Alliance
The Atlas V is one of two launch vehicles
developed as part of the U.S. Air Force’s Evolved
Expendable Launch Vehicle (EELV) program in the
late 1990s. The Atlas V was developed by the
Lockheed Martin Corporation; since December
2006 it has been produced by United Launch
Alliance (ULA), a joint venture between The
Boeing Company and
Lockheed Martin. The Atlas
V is made available for com-
mercial launches by
Lockheed Martin
Commercial Launch
Services.
The Atlas V is available
in the 400 and 500 series and
accommodates 4-meter
(13.1-foot) and 5.4-meter
(17.6-foot) fairings and up to
five strap-on solid rocket
motors. The Atlas 400 series
can place payloads between 4,950 and 7,640 kilo-
grams (10,910 and 16,843 pounds) into geosyn-
chronous transfer orbit (GTO). The Atlas 500 series
can place payloads between 3,970 and 8,670 kilo-
grams (8,750 and 19,120 pounds) into GTO. The
Atlas V launches out of Cape Canaveral Air Force
Station (CCAFS) in Florida and Vandenberg Air
Force Base (VAFB) in California.
Since its introduction in 2002 the Atlas V has
performed 12 launches. In 2007 four Atlas V
launches took place, all non-commercial. On a June
15 launch, the vehicle placed the classified NRO L-
30 payload into a lower-than-planned orbit. The
divergence from the planned orbit was traced to a
leaky fuel valve in the Centaur upper stage that
caused the Centaur engine to shut down early. That
valve has been replaced with a proven older
model.12 Up to seven Atlas V launches, including
one commercial mission, are planned for 2008.
Delta II – United Launch Alliance
The Delta II launch vehicle, in service since
1989, traces its heritage to the Thor missile pro-
gram of the 1950s. Since
December 2006 the Delta II
has been produced by ULA,
and is marketed commercial-
ly by Boeing Launch
Services (BLS). The Delta II
has the capability to launch
payloads of 900 to 2,170
kilograms (1,980 to 4,790
pounds) to GTO, and 2,700
to 6,100 kilograms (5,960 to
13,440 pounds) to low Earth
orbit (LEO), and can launch
from either CCAFS or
VAFB.
There were eight Delta II launches in 2006,
including commercial launches of the Cosmo-
Skymed 1, WorldView-1, and Cosmo-Skymed 2
satellites in June, September, and December,
respectively, from VAFB. As many as nine Delta II
launches, including three commercial missions, are
planned for 2008.
Federal Aviation Administration Office of Commercial Space Transportation 9
2008 U.S. Commercial Space Transportation Developments and Concepts Expendable Launch Vehicles
Expendable Launch Vehicles
Atlas V
Delta II
Delta IV – United Launch Alliance
The Delta IV is one of two launch vehicles
developed for the EELV program in the 1990s. The
Delta IV was designed by Boeing, and since
December 2006 has been produced by ULA.
Originally developed for both commercial and
government applications, the Delta IV is currently
marketed only to U.S. government customers.
The Delta IV is available in five versions,
four Medium versions, with varying payload fairing
sizes and number of strap-on boosters, and one
Heavy version, which uses three
common booster core stages
instead of one. Payload capacities
to LEO range from 9,150 kilo-
grams (20,170 pounds) for the
Medium to 22,560 kilograms
(49,740 pounds) for the Heavy.
Geosynchronous transfer orbit
capacities range from 4,300 to
12,980 kilograms (9,480 to 28,620
pounds). The Delta IV operates
from CCAFS and VAFB.
10 Federal Aviation Administration Office of Commercial Space Transportation
Delta IV Heavy
Expendable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
MMeeddiiuumm
VVeehhiiccllee Minotaur Pegasus XL Taurus XL Delta II Delta IV Atlas V Delta IV Heavy Zenit-3SL
CCoommppaannyyOrbital
SciencesOrbital
SciencesOrbital
SciencesULA ULA ULA ULA Sea Launch
FFiirrsstt LLaauunncchh 2000 1990 1994 1990 2002 2002 2004 1999
9,150 kg(20,170 lb)(Delta IV M)
12,500 kg(27,560 lb)
(Atlas V 402)
13,360 kg(29,440 lb)
(Delta IV M+ (5,4))
20,520 kg (45,240 lb)
(Atlas V 552)
7,510 kg (16,550 lb)(Delta IV M)
7,095 kg (15,640 lb)
(Atlas V 402)
11,300 kg(24,920 lb)
(Delta IV M+ (5,4))
14,095 kg(31,075 lb)
(Atlas V 552)
4,300 kg (9,480 lb)
(Delta IV M)
4,950 kg (10,910 lb)
(Atlas V 401)
7,020 kg (15,470 lb)
(Delta IV M+ (5,4))
8,670 kg (19,120 lb)
(Atlas V 551)
12,980 kg (28,620 lb)
6,100 kg (13,500 lb)
CCAFS, VAFB CCAFS, VAFBPacific Ocean
22,560 kg (49,740 lb)
N/A
22,560 kg (49,740 lb)
N/A
2
IInntteerrmmeeddiiaattee HHeeaavvyy
2 2 3
CCAFS, VAFB
SSmmaallll
34
1,590 kg(3,505 lb)
860 kg(2,000 lb)
(SSO)
VAFB
430 kg(950 lb)
CCAFS, VAFB
6,100 kg(13,440 lb)
VAFB, Wallops
SSttaaggeess 4 3
640 kg(1,410 lb)
440 kg(970 lb)
PPaayyllooaadd PPeerrffoorrmmaannccee
((LLEEOO))
2,170 kg(4,790 lb)
3,600 kg(7,930 lb)
PPaayyllooaadd PPeerrffoorrmmaannccee
((LLEEOO ppoollaarr))
LLaauunncchh SSiitteess
340 kg(750 lb)
(SSO)
190 kg(420 lb)
(SSO)
VAFB, Wallops, CCAFS
PPaayyllooaadd PPeerrffoorrmmaannccee
((GGTTOO))N/A N/A
Table 1: Currently Available Expendable Launch Vehicles
The Delta IV has flown seven times since its intro-
duction in late 2002. One Delta IV Heavy launch,
of the DSP 23 satellite, took place in 2007. Up to
four Delta IV launches, including one FAA-licensed
mission, are planned for 2008.
Minotaur I – Orbital Sciences Corporation
Under the U.S. Air
Force’s Orbital/Suborbital
Program (OSP), Orbital
Sciences Corporation has
developed the Minotaur fam-
ily of launch vehicles, start-
ing with the Minotaur I, to
launch small government
payloads. The Minotaur I
booster uses a combination
of rocket motors from
decommissioned Minuteman
2 ICBMs and upper stages
from Orbital’s Pegasus
launch vehicle. The first two
stages of the Minotaur are Minuteman 2 M-55A1
and SR-19 motors, while the upper two stages are
Orion 50 XL and Orion 38 motors from the Pegasus
XL.
The Minotaur I entered service in 2000 and
has performed seven launches to date, including the
launch of the NFIRE satellite in 2007 from the
Mid-Atlantic Regional Spaceport (MARS) in
Virginia. A Minotaur I is scheduled to launch the
TacSat-3 satellite in 2008, also from MARS. The
Minotaur I has previously performed launches from
VAFB, and can operate from CCAFS and Kodiak
Launch Complex, Alaska.
Pegasus XL – Orbital Sciences Corporation
The Pegasus XL is an air-launched booster
designed for small payloads, primarily to low Earth
and sun-synchronous orbits. Introduced in 1994, the
Pegasus XL is a derivative of the original Pegasus
rocket, with stretched first and second stages. (The
original Pegasus, first launched in 1990, was retired
in 2000.) The Pegasus XL, with three solid-propel-
lant stages and an optional hydrazine monopropel-
lant upper stage, is deployed from an Orbital
Sciences L-1011 aircraft named “Stargazer.” The
air-launched nature of the Pegasus XL allows mis-
sions to be staged from a variety of sites, including
Edwards Air Force Base (EAFB) and VAFB in
California; CCAFS and KSC in Florida; NASA
Wallops Flight Facility (WFF) in Virginia;
Kwajalein Missile Range, Marshall Islands; and
Gando Air Force Base (GAFB), Canary Islands.
The Pegasus XL performed one launch in
2007, launching NASA’s Aeronomy of Ice in the
Mesosphere (AIM) mission out of VAFB. Two
Pegasus XL missions are scheduled for 2008.
Taurus – Orbital Sciences Corporation
The Taurus is a ground-
launched vehicle based on
the air-launched Pegasus.
Orbital Sciences developed
the Taurus under the sponsor-
ship of the Defense
Advanced Research Projects
Agency (DARPA). The goal
was to develop a standard
launch vehicle that could set
up quickly in new locations
and launch small satellites
that are too large for the
Pegasus XL. The Taurus uses
the three stages of a Pegasus
(without wings or stabilizers)
stacked atop a Castor 120
solid rocket motor. The
Castor 120 serves as the first
stage of the Taurus. The
Taurus is available in standard and XL versions.
The Taurus successfully completed six of seven
launch attempts since entering service in 1994. No
Taurus launches took place in 2007, but two are
scheduled for 2008.
Zenit-3SL – Sea Launch Company, LLC
The Zenit-3SL is a Ukrainian-Russian launch
vehicle operated by Sea Launch Company, LLC, a
multinational joint venture featuring four partners.
Federal Aviation Administration Office of Commercial Space Transportation 11
2008 U.S. Commercial Space Transportation Developments and Concepts Expendable Launch Vehicles
Minotaur I
Pegasus XL
Taurus
Ukrainian sister companies SDO Yuzhnoye and PO
Yuzhmash provide the first two stages, the same as
those used on the Zenit 2 launch vehicle. A Russian
company, RSC Energia, provides the third stage, a
Block DM-SL upper stage. The Norwegian ship-
building company, Aker, designed and built the two
Sea Launch vessels and contracts marine opera-
tions. The Boeing Company provides the payload
fairing and interfaces, as well as operations and
business management.
The Zenit-3SL launches from the Odyssey
Launch Platform, which travels from its Sea
Launch Home Port in Long Beach, California, to a
position on the equator in the Pacific Ocean for
each mission. Launch operations are remotely con-
trolled from a separate vessel, the Sea Launch
Commander, which is positioned approximately 6.5
kilometers (about 4 miles) uprange from the plat-
form during launch operations. Sea Launch con-
ducts commercial launches with a license from
FAA. Under current U.S. space transportation poli-
cy, the mostly foreign-manufactured Zenit-3SL
vehicle is not available for
launch of U.S. government
payloads.
The first Zenit-3SL
launch of 2007 ended in fail-
ure on January 30 when the
vehicle lost thrust moments
after ignition of the first
stage engine, destroying the
vehicle and its payload, the
NSS-8 satellite. An investiga-
tion concluded that metallic
debris became lodged in the
liquid oxygen turbopump in
the engine, initiating com-
bustion in the chamber, and leading to the destruc-
tion of the engine and launch vehicle.13 The Sea
Launch team has since taken measures to prevent
the problem from recurring, and also repaired and
recertified the Odyssey, which suffered minor dam-
age, including the loss of its flame deflector. The
Zenit-3SL is scheduled to return to flight with the
launch of the Thuraya-3 satellite in January 2008,
part of a full manifest of up to five launches sched-
uled for the year.14
ELV Development Efforts
A number of efforts by both established cor-
porations and startups are currently in progress to
develop new ELVs. The majority of these designs
focus on the small LEO payload sector of the
launch market, and reducing launch costs is a key
goal.
ALV – Alliant Techsystems
In October 2006, ATK of Edina, Minnesota,
announced it was developing a small launch vehi-
cle, the ATK Launch Vehicle (ALV). The ALV is
based on existing rocket stages developed by the
company. ATK carried out a successful “pathfinder”
for the ALV by assembling the vehicle on the pad at
MARS in 2006. The first
launch of the two-stage ALV,
a suborbital flight designated
ALV X-1 and carrying two
NASA experimental hyper-
sonic and reentry research
payloads, is scheduled for
2008 from MARS in
Virginia. ATK plans to offer
a larger orbital version of the
ALV for government and
commercial customers seek-
ing responsive launches of
small satellites in 2010 and
beyond.15
Aquarius – Space Systems/Loral
Space Systems/Loral of Palo Alto, California,
has proposed Aquarius, a low-cost launch vehicle
designed to carry small, inexpensive payloads into
LEO. This vehicle’s mission will consist primarily
of launching inexpensive-to-replace bulk products,
such as water, fuel, and other consumables, into
space. As currently designed, Aquarius will be a
single-stage vehicle 43 meters (141 feet) high and 4
12 Federal Aviation Administration Office of Commercial Space Transportation
VVeehhiiccllee:: ATK Launch Vehicle
DDeevveellooppeerr:: Alliant Techsystems
FFiirrsstt LLaauunncchh:: 2008 (suborbital); 2010 (orbital)
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 1,360 kg (3,000 lb) suborbital
LLaauunncchh SSiittee:: MARS
MMaarrkkeettss SSeerrvveedd:: Responsive launches of small satel-lites for civil, commercial, and military customers
Expendable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
Zenit 3SL
ALV
meters (13.1 feet) in diameter, powered by a single
engine using liquid hydrogen and oxygen propel-
lants. The vehicle is floated in the ocean before
launch to minimize launch infrastructure and will
be able to place a 1,000-kilogram (2,200-pound)
payload into a
200-kilometer
(125-mile), 52-
degree orbit.
Located in the
base of the vehi-
cle, the payload
will be extracted
by an orbiting
space tug for
transfer to its
ultimate destina-
tion. When used
for small satel-
lite launch,
Aquarius can dispense multiple satellites into 200-
kilometer (125-mile) orbits at any desired inclina-
tion. It can do this because launching at appropriate
ocean locations virtually eliminates range con-
straints on the trajectory. After payload deployment
is completed, the vehicle will de-orbit and be
destroyed. Planned launch costs are $1-2 million
per flight.
Previous work on Aquarius includes a study
of the launch concept funded by the California
Space Authority in 2002. Space Systems/Loral, in
conjunction with Aerojet, a GenCorp Company
based in Sacramento, California, and ORBITEC of
Madison, Wisconsin, has performed studies on a
vortex combustion cold wall engine, using LOX
and liquid hydrogen propellants that would be used
on Aquarius. Research on the Aquarius concept
includes studies of propellant transfer, analyses of
floating launch, and development and testing of an
engine with 133,000 to 445,000 newtons (30,000 to
100,000 pounds-force) of thrust.16
Eagle S-series – E’Prime Aerospace Corporation
E’Prime Aerospace of Falls Church, Virginia,
is developing a family of launch vehicles, called the
Eagle S-series, based on the LGM-118A
Peacekeeper ICBM design. Like the Peacekeeper,
this vehicle will be ejected from a ground-based
silo, using a compressed gas system. At an altitude
of 61 meters (200 feet), the engines will ignite. The
smallest vehicle, the Eaglet, could launch 580 kilo-
grams (1,280 pounds) into LEO. A somewhat larger
version, the Eagle, could put 1,360 kilograms
(3,000 pounds) into LEO.
Both vehicles will use solid
propellant lower stages and
liquid propellant upper
stages. E’Prime has also pro-
posed larger vehicles, desig-
nated S-1 through S-7, with
the ability to place consider-
ably larger payloads into
LEO and to add a geosyn-
chronous Earth orbit (GEO)
capability. The Eagle S-series
concept dates back to 1987
when the company signed a
commercialization agreement
Federal Aviation Administration Office of Commercial Space Transportation 13
2008 U.S. Commercial Space Transportation Developments and Concepts Expendable Launch Vehicles
VVeehhiiccllee:: Aquarius
DDeevveellooppeerr:: Space Systems/Loral
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 1,000 kg (2,200 lb) to LEO (52º)
LLaauunncchh SSiittee:: TBD
MMaarrkkeettss SSeerrvveedd:: ISS and spacecraft resupply, smallsatellite launch
Aquarius mission profile
Aquarius
Eaglet and Eagle
VVeehhiiccllee:: Eaglet/Eagle
DDeevveellooppeerr:: E’Prime Aerospace
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 580 kg (1,280 lb) to LEO(Eaglet); 1,360 kg (3,000 lb) to LEO (Eagle)
LLaauunncchh SSiittee:: MARS
MMaarrkkeettss SSeerrvveedd:: Small satellite launch
with the U.S. Air Force to use Peacekeeper technol-
ogy for commercial launch vehicles. In August
2007 E’Prime Aerospace announced that it had
selected MARS as its primary launch site and will
develop infrastructure there to support its vehicles.
The company also started the process of obtaining a
launch license from FAA, and in November 2007
was notified that the application had cleared an
interagency policy review, removing any govern-
ment obstacles to its use of its Peacekeeper-derived
motors.17
FALCON SLV – Lockheed Martin Michoud Operations
Lockheed Martin Michoud Operations of New
Orleans, Louisiana, was awarded one of four
DARPA Force Application and Launch from
CONUS (FALCON) contracts in September 2004.
This $11.7 million contract tasks Lockheed Martin
to develop concepts for a low-cost launch vehicle.
Lockheed Martin’s FALCON SLV approach uses
all-hybrid propulsion and a mobile launch system
that can launch from an unimproved site with limit-
ed infrastructure on 24 hours notice, placing up to
840 kilograms (1,855
pounds) into LEO. In
2005, Lockheed conduct-
ed two test firings of the
hybrid rocket motor that
will be used on the upper
stage of the SLV. Though
Lockheed did not win a
Phase 2B Falcon contract
from DARPA in late
2005, the company con-
tinues work on the FALCON SLV, focusing on the
development and testing of the second stage of the
vehicle.18
Nanosat Launch Vehicle – Garvey Spacecraft Corporation
Garvey Spacecraft Corporation (GSC), based
in Long Beach, California, is a small research and
development (R&D) company, focusing on the
development of advanced space technologies and
launch vehicle systems. As part of the California
Launch Vehicle Initiative (CALVEIN), GSC and
California State University, Long Beach (CSULB)
jointly conduct preliminary R&D tasks to establish
the foundation for development of a two-stage, liq-
uid propellant, Nanosat Launch Vehicle (NLV).
Capable of delivering 10 kilograms (22 pounds) to
a 250-kilometer (155-mile) polar orbit, the NLV
will provide low-cost, dedicated launch services to
universities and other research organizations that
traditionally depend on secondary payload opportu-
nities to access space. Their current work builds
upon flights that the team
conducted using several of
its LOX/ethanol Prospector
research vehicles. The com-
pany’s most visible accom-
plishments include the first-
ever flight of a composite
LOX tank, conducted in part-
nership with Microcosm,
Incorporated; the first-ever
powered flights of a liquid-
propellant aerospike engine;
and the launch and 100 per-
cent recovery of several pro-
totype reusable test vehicles.
On September 15, 2007, the GSC/CSULB
team launched the Prospector 8A (P-8A) rocket
from the Mojave Desert in California. The rocket
featured the first flight of a new 20,000-newton
(4,500-pounds-force) engine designed for future
prototypes of the NLV. The loss of the P-8A’s tail
fins four seconds into the flight caused the vehicle
to tumble out of control.19 GSC is incorporating
14 Federal Aviation Administration Office of Commercial Space Transportation
VVeehhiiccllee:: Nanosat Launch Vehicle
DDeevveellooppeerr:: Garvey Spacecraft Corporation
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 10 kg (22 lb) to LEO (polar orbit)
LLaauunncchh SSiittee:: TBD
MMaarrkkeettss SSeerrvveedd:: Nanosatellite launch
Expendable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
VVeehhiiccllee:: FALCON SLV
DDeevveellooppeerr:: Lockheed Martin Michoud Operations
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 840 kg (1,855 lb) to LEO
LLaauunncchh SSiittee:: TBD
MMaarrkkeettss SSeerrvveedd:: Small satellite launch, responsivespace operations
FALCON SLV
Prospector 8A
design lessons from that flight into its next vehicle,
the Prospector 9 (P-9), currently under development
under a Phase 2 Small Business Innovation
Research from the USAF. GSC and its research
partner, CSULB, plan five launches in the next year
of the P-9 and two other vehicles, Prospectors 10
and 12.20
Sprite SLV – Microcosm, Inc.
Microcosm, Incorporated, of Hawthorne,
California, has been developing the Scorpius family
of ELVs. Several versions are under consideration,
and two prototype suborbital test models, SR-S and
SR-XM-1, flew successfully from White Sands
Missile Range, New
Mexico, in 1999 and
2001, respectively.
Eventually, Microcosm
plans to market up to
five Scorpius variants.
Each Scorpius variant is
based on a scalable mod-
ular design featuring
simple, LOX/Jet-A, pres-
sure-fed engines without
turbopumps and low-cost avionics equipped with
GPS/INS (global positioning system/inertial naviga-
tion system). The thick propellant tanks provide
added durability during flight and ground handling.
The orbital variants have three stages.
The suborbital variant, the SR-M, which is
essentially one of seven nearly identical “pods” of
the Sprite orbital vehicle, has been built and has a
maximum payload of 1,089 kilograms (2,400
pounds). Four orbital variants are planned. The
Sprite Small Launch Vehicle (SLV) is projected to
loft up to 481 kilograms (1,060 pounds) to LEO.
Microcosm's light-, medium-, and heavy-lift
Scorpius variants will deploy payloads to LEO and
to GTO with an upper stage. The Liberty Light-Lift
vehicle would loft up to 1,924 kilograms (4,240
pounds) to LEO and up to 757 kilograms (1,670
pounds) to GTO. The Exodus Medium-Lift vehicle
would deploy up to 8,938 kilograms (19,700
pounds) to LEO and up to 3,518 kilograms (7,760
pounds) to GTO. Specifications for the heavy-lift
Space Freighter are not yet available.
Microcosm received one of four contracts,
valued at $10.5 million, from DARPA in September
2004 for Phase 2 of the Falcon small launch vehicle
program to support development of the Eagle SLV.
However, the company was notified in August 2005
that it had not been selected for further work on the
program. The company had been continuing devel-
opment of the Scorpius vehicle concept under a
separate DoD contract, but that funding ran out in
September 2006, forcing Microcosm to work on the
project under corporate funding, which continues at
present, while looking for additional funding to
restart development of the Sprite SLV.21
Minotaur IV and V – Orbital Sciences Corporation
Under a contract with the USAF Space and
Missile Systems Center, Orbital Sciences Corporation is
currently developing the Minotaur IV launch vehi-
cle for U.S. government payloads. The Minotaur IV
is derived from the Peacekeeper ICBM, using three
Peacekeeper solid-propellant
stages and an Orion 38 motor
for the fourth stage. The
Minotaur IV uses a standard
234-centimeter (92-inch)
payload fairing also used on
Orbital’s Taurus rocket. The
first Minotaur IV launch is
scheduled for late 2008,
when it will launch the Space-Based Surveillance
System (SBSS) satellite for the USAF.
Federal Aviation Administration Office of Commercial Space Transportation 15
2008 U.S. Commercial Space Transportation Developments and Concepts Expendable Launch Vehicles
VVeehhiiccllee:: Eagle SLV
DDeevveellooppeerr:: Microcosm, Inc.
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 3
PPaayyllooaadd PPeerrffoorrmmaannccee:: 481 kg (1,060 lb) to LEO
LLaauunncchh SSiittee:: VAFB, WFF, CCAFS
MMaarrkkeettss SSeerrvveedd:: Small satellite launch, responsivespace operations
Sprite SLV
VVeehhiiccllee:: Minotaur IV and V
DDeevveellooppeerr:: Orbital Sciences Corporation
FFiirrsstt LLaauunncchh:: 2008 (Minotaur IV); TBD (Minotaur V)
NNuummbbeerr ooff SSttaaggeess:: 4 (Minotaur IV); 5 (Minotaur V)
PPaayyllooaadd PPeerrffoorrmmaannccee:: 1,750 kg (3,860 lb) to LEO(Minotaur IV); 675 kg (1,495 lb) to GTO (Minotaur V)
LLaauunncchh SSiittee:: MARS, VAFB
MMaarrkkeettss SSeerrvveedd:: Small satellite launch and responsivespace operations for U.S. government-sponsored pay-loads
Minotaur IV
Orbital is also developing a derivative of the
Minotaur IV, called the Minotaur V, for payloads
launched to orbits beyond LEO. The Minotaur V
features the same three Peacekeeper-based lower
stages, but uses a Star 48 fourth stage and Star 37
fifth stage, allowing it to put 678 kilograms (1,495
pounds) into GTO and 440 kilograms (970 pounds)
on a translunar injection trajectory. The Minotaur V
shares many of the same subsystems as the
Minotaur IV, requiring only an additional $10 mil-
lion in non-recurring engineering expenses to com-
plete its development.22
QuickReach – AirLaunch LLC
AirLaunch LLC, based in Kirkland,
Washington, is leading the development of a small,
low-cost, air-launched vehicle for defense and other
applications. The two-stage rocket is carried aloft
inside a cargo aircraft, such as a C-17A or other
large cargo aircraft. The rocket is released from the
aircraft at an altitude of
7,600 to 10,700 meters
(25,000 to 35,000 feet)
and fires its liquid-pro-
pellant engines to ascend
to orbit. The vehicle is
designed to place a 450-
kilogram (1,000-pound)
payload into LEO for
less than $5 million,
with a response time of
less than 24 hours.
In July 2006, AirLaunch LLC conducted the
safe release of a full-scale dummy rocket from an
Air Force C-17 cargo airplane. The demonstration
was a follow-on to two prior drop tests. AirLaunch
LLC did not perform further drop tests in 2007.
During 2007 AirLaunch completed work on
Phase 2B of the DARPA/USAF Falcon small
launch vehicle program, including numerous tests
of its liquid oxygen/propane vapor pressurization
(VaPak) system. AirLaunch achieved the longest-
ever burn of a VaPak engine system with a 191-sec-
ond engine firing on a test stand at Mojave Air and
Space Port, California, in April 2007. In June 2007
AirLaunch received a $7.6-million contract for
Phase 2C of the Falcon program. The contract cov-
ers continued development and testing of the VaPak
system.23 Phase 2 is anticipated to conclude with the
test launch of a QuickReach rocket in approximate-
ly 2010.24
Taurus 2 – Orbital Sciences Corporation
In 2007, Orbital Sciences Corporation
announced that it had begun a study of a new
launch vehicle, the Taurus 2, designed to serve
medium-class payloads for U.S. government and
commercial customers. The Taurus 2’s first stage
would be powered by a pair of Aerojet AJ26-58
engines, a version of the NK-33 engine developed
for the Soviet Union’s N-1 lunar rocket in the
1960s; Orbital has not disclosed any information
about the vehicle’s upper stages. The Taurus 2
would be able to place 6,000 kilograms (13,225
pounds) into LEO and 3,700 kilograms (8,150
pounds) into sun-synchronous orbit. Enhanced ver-
sions of the Taurus 2 could be used to launch pay-
loads of up to 3,000 kilograms (6,600 pounds) into
GEO. Orbital plans to make a decision on develop-
ing the Taurus 2 in 2008, with the first launch pro-
jected to occur in mid-2010.25
Z-1 – Zig Aerospace, LLC
Zig Aerospace of King George, Virginia, is
developing the Z-1 small launch vehicle. Intended
to launch nanosatellites and similar small payloads,
Z-1 has a maximum payload capacity of five kilo-
grams (11 pounds) to LEO. The two-stage vehicle,
powered by hybrid propellants, is intended to cost
less than $200,000 per launch. Zig Aerospace is in
16 Federal Aviation Administration Office of Commercial Space Transportation
Expendable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
VVeehhiiccllee:: QuickReach
DDeevveellooppeerr:: AirLaunch LLC
FFiirrsstt LLaauunncchh:: 2010
NNuummbbeerr ooff SSttaaggeess:: 3 (including the launch aircraft)
PPaayyllooaadd PPeerrffoorrmmaannccee:: 450 kg (1,000 lb) to LEO
LLaauunncchh SSiittee:: Air launched
MMaarrkkeettss SSeerrvveedd:: Small satellite launch, responsivespace operations
QuickReach
VVeehhiiccllee:: Taurus 2
DDeevveellooppeerr:: Orbital Sciences Corporation
FFiirrsstt LLaauunncchh:: 2010
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 6,000 kg (13,225 lb) to LEO
LLaauunncchh SSiittee:: TBD
MMaarrkkeettss SSeerrvveedd:: Medium-class payloads for governmentand commercial customers
the midst of a 3-year development program. Once
the Z-1 vehicle enters operations, the company
expects to be able to conduct launches as frequently
as once a month.26
Zenit-3SLB – Sea Launch Company, LLC, and Space
International Services
The Sea Launch Board of Directors voted on
September 30, 2003, to offer launch services from
the Baikonur Space Center in Kazakhstan, in addi-
tion to its sea-based launches at the Equator. The
new offering, Land Launch, is based on the collab-
oration of Sea Launch Company and Space
International Services, of Russia, to meet the launch
needs of commercial customers with medium
weight satellites. The Land Launch system uses a
version of the Sea Launch Zenit-3SL rocket, the
Zenit-3SLB, to lift commercial satellites in the
2,000 to 3,600-kilogram (4,410 to 7,940-pound)
range to GTO and heavier
payloads to inclined or lower
orbits. The three stages on
the Zenit-3SLB are the same
as those on the Sea Launch
Zenit-3SL; the fairing is the
only significant difference
between the two vehicles. A
two-stage configuration of
the same rocket, the Zenit-
2SLB, is also available for
lifting heavy payloads, or
groups of payloads, to LEO.
Payloads and vehicles will be processed and
launched from existing Zenit facilities at the
Baikonur launch site. The first Land Launch mis-
sion is scheduled for 2008. To date, Sea Launch,
which manages marketing and sales for this new
offering (in addition to its sea-based missions), has
received seven commercial orders for the Land
Launch service.27
NASA Exploration Launch Vehicles
On September 19, 2005, NASA announced its
planned mission architecture for crewed lunar mis-
sions. The plan calls for the development of two
new launch vehicles, the Crew Launch Vehicle
(since renamed the Ares I) and the Cargo Launch
Vehicle (renamed the Ares V). Both vehicles are
designed to leverage Shuttle and even Apollo-era
technologies to launch crewed and uncrewed space-
craft required to carry out the Vision for Space
Exploration.
Ares I
The Ares I Crew Launch Vehicle is a two-
stage vehicle designed principally to launch
NASA’s Orion CEV into LEO and may also be
used to launch cargo spacecraft to the ISS. The first
stage of the Ares I is a five-segment reusable solid
rocket motor (RSRM) derived from the four-seg-
ment boosters used in the Space Shuttle program.
The second stage is a
new design powered by
a single J-2X engine,
based on the J-2S engine
developed at the end of
the Apollo program in
the early 1970s; it uses
LOX and liquid hydro-
gen propellants. The
Orion spacecraft, along
with an escape rocket,
will be mounted on top
of the second stage.
Federal Aviation Administration Office of Commercial Space Transportation 17
2008 U.S. Commercial Space Transportation Developments and Concepts Expendable Launch Vehicles
VVeehhiiccllee:: Zenit-3SLB
DDeevveellooppeerr:: Space International Services
FFiirrsstt LLaauunncchh:: 2008
NNuummbbeerr ooff SSttaaggeess:: 3
PPaayyllooaadd PPeerrffoorrmmaannccee:: 3,600 kg (7,940 lb) to GTO
LLaauunncchh SSiittee:: Baikonur
MMaarrkkeettss SSeerrvveedd:: Commercial GEO satellite launch
VVeehhiiccllee:: Ares I
DDeevveellooppeerr:: NASA
FFiirrsstt LLaauunncchh:: 2009 (suborbital); 2014 (orbital)
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 22,700 kg (50,000 lb) to LEO
LLaauunncchh SSiittee:: KSC
MMaarrkkeettss SSeerrvveedd:: Crew launches for exploration and ISSmissions
VVeehhiiccllee:: Z-1
DDeevveellooppeerr:: Zig Aerospace, LLC
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 5 kg (11 lb) to LEO
LLaauunncchh SSiittee:: TBD
MMaarrkkeettss SSeerrvveedd:: Nanosatellite launch, responsive spaceoperations
Zenit-3SLB Ares I
Development of the Ares I is currently in
progress. In July 2007 NASA awarded Pratt &
Whitney Rocketdyne a $1.2-billion contract for the
J-2X engine.28 In August 2007, NASA selected
Boeing to build the upper stage of the Ares I.29
NASA also awarded Boeing a contract in December
2007 for the instrument unit avionics for the Ares I,
the last major component of the launch vehicle to
be assigned to a contractor.30 The first test flight of
the Ares I, designated Ares I-X and planned for
2009, will be a suborbital launch with an inert sec-
ond stage. The Ares I is scheduled to enter service
no later than 2014.
Ares V
The Ares V Cargo Launch Vehicle is a two-
stage, heavy-lift vehicle that NASA will use to
carry out human missions to the Moon and other
destinations. The Ares V uses two, five-segment
RSRMs similar to those developed for the Ares I
vehicle, attached to either side of a core propulsion
stage. The core stage
features five RS-68
engines, the same LOX
and liquid hydrogen
engines as those now
used on the Delta IV
family of vehicles.
Under the current explo-
ration architecture, an
Ares V vehicle would
place a lunar module and Earth departure stage into
LEO, where the module would dock with an Orion
spacecraft launched separately by an Ares I. The
combined vehicle would then leave Earth orbit for
the Moon. Detailed development of the Ares V is
not expected to begin until the end of the decade.
Sounding Rockets
In addition to orbital launch vehicles, a num-
ber of suborbital ELVs, or sounding rockets, are in
use today. These vehicles, which primarily use solid
propellants, support a variety of applications,
including astronomical observations, atmospheric
research, and microgravity experiments.
Black Brant – Bristol Aerospace Limited
Over 1,000 Black Brant rockets have been
launched since 1962, when manufacturing of the
vehicle began. Versions of the Black Brant can
carry payloads ranging from 70 to 850 kilograms
(154 to 1,874 pounds) to altitudes from 150 to more
than 1,500 kilometers (93 to 932 miles), and can
provide up to 20 minutes of microgravity time dur-
ing a flight. The Black Brant and Nikha motors
used on some Black Brant versions are manufac-
tured in Canada by Bristol Aerospace Limited (a
Magellan Aerospace Company). Terrier, Talos, and
Taurus motors used on other Black Brant versions
are built in the United States. The launch operator
integrates these vehicles. In the United States,
NASA has been a frequent user of Black Brant
vehicles.
The smallest version of the Black Brant fami-
ly is the single-stage Black Brant 5, which is 533
centimeters (210 inches) long and 43.8 centimeters
(17.24 inches) in diameter. The rocket produces an
average thrust of 75,731 newtons (17,025 pounds-
force). The Black Brant 5
motor is used as the second
or third stage in larger, multi-
stage versions of the Black
Brant. The most powerful of
the line, Black Brant 12, is a
four-stage vehicle that uses
the Black Brant 5 motor as
its third stage. This vehicle
can launch a 113-kilogram
(250-pound) payload to an
altitude of at least 1,400 kilo-
meters (870 miles), or a 454-
kilogram (1,000-pound) pay-
load to an altitude of at least
400 kilometers (250 miles).31
Oriole – DTI Associates
SPACEHAB’s Astrotech Space Operations
developed the Oriole sounding rocket in the late
1990s to provide launch services for commercial
and scientific payloads. Oriole was both the first
privately-developed sounding rocket in the United
States and the first new U.S. sounding rocket in 25
18 Federal Aviation Administration Office of Commercial Space Transportation
Expendable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
VVeehhiiccllee:: Ares V
DDeevveellooppeerr:: NASA
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 131,500 kg (290,000 lb) to LEO
LLaauunncchh SSiittee:: KSC
MMaarrkkeettss SSeerrvveedd:: Cargo launches for exploration missions
Ares V
Black Brant
years. The Oriole is a single-stage vehicle with a
graphite-epoxy motor manufactured by Alliant
Missile Products Company of Rocket Center, West
Virginia. It is 396 centimeters (156 inches) long, 56
centimeters (22 inches) in diameter, and generates
an average thrust of 92,100 newtons (20,700
pounds-force). The vehicle provides payloads with
six to nine minutes of microgravity during flight.
Additionally, it can be combined with other motors
to create two-stage sounding rockets, with the
Oriole serving as the second stage.
The first Oriole launch took place from
NASA WFF on July 7, 2000. That launch used a
two-stage configuration, with the Oriole serving as
the second stage and a Terrier Mk 12 motor serving
as the first stage. The Oriole
sounding rocket reached a
peak altitude of 385.6 kilo-
meters (229 miles) 315 sec-
onds after launch during the
ten-minute test flight. In July
2001, SPACEHAB’s
Astrotech Space Operations
sold the Oriole program to
DTI Associates of Arlington,
Virginia, which integrates the
vehicle and offers it commer-
cially. A production run of 15
Oriole rockets was scheduled
for delivery in late 2007.
Terrier-Orion – DTI Associates
The Terrier-Orion is a two-stage, spin-stabi-
lized sounding rocket, which uses a Terrier Mk 12
Mod 1 engine for its first stage and an improved
Orion motor for its second stage. The Terrier Mk 12
Mod 1 is a surplus U.S. Navy missile motor; Orion
is a surplus U.S. Army missile motor. The Terrier-
Orion is 10.7 meters (35.1 feet) long. The Terrier
stage is 46 centimeters (18 inches) in diameter, and
the Orion is 36 centimeters (14 inches) in diameter.
The Terrier-Orion can loft payloads weighing up to
290 kilograms (640 pounds) to altitudes up to 190
kilometers (118 miles).
A more powerful version of the Terrier-Orion
rocket uses the Terrier Mk 70 motor as its first
stage. This version was used for two FAA-licensed
suborbital launches performed by Astrotech Space
Operations/DTI at the Woomera Instrumented
Range in Australia in 2001
and 2002. The third flight, in
July 2002, successfully flew
the HyShot scramjet engine
experiment. DTI Associates
of Arlington, Virginia, now
markets and offers integra-
tion services for the Terrier-
Orion after purchasing all
intellectual property rights to
the rocket from SPACEHAB
in July 2001. Six Terrier-
Orion rockets were launched
in 2006.
Hybrid Sounding Rocket Program – LockheedMartin-Michoud
Lockheed Martin-Michoud is developing a
hybrid sounding rocket (HYSR) program with
NASA Marshall Space Flight Center (MSFC). A
Space Act Agreement between NASA MSFC and
Lockheed Martin-Michoud Operations enabled col-
laboration on this new technology. Development
ground testing (hardware qualification) occurred at
NASA Stennis Space Center between 2000 and
2001. This testing concluded with a successful
demonstration flight of a prototype sounding rocket
from NASA WFF in December 2002. The flight
demonstration vehicle was a 17-meter (57-foot)
long sounding rocket using liquid oxygen and solid
fuel, a rubberized compound known as hydroxyl
terminated polybutadiene (HTPB). The rocket gen-
erated 267,000 newtons (60,000 pounds-force) of
thrust during a burn time of 31 seconds, and
reached an altitude of approximately 43 miles.
In 2004, further testing of the HYSR motors
occurred at NASA Stennis Space Center. These
tests demonstrated the structural integrity of
Lockheed Martin-Michoud’s fuel-grain design and
are facilitating development of advanced state-of-
the-art hybrid rocket motors.
Hybrid Test Rocket – Lockheed Martin-Michoud and Nammo AS
Lockheed Martin-Michoud partnered with a
Norwegian company, Nammo Raufoss AS, to build
the Hybrid Test Rocket (HTR), a single-stage
hybrid-propulsion sounding rocket. Lockheed
Martin-Michoud provided the design, engineering
schematics, and vehicle assembly plan, with the
Federal Aviation Administration Office of Commercial Space Transportation 19
2008 U.S. Commercial Space Transportation Developments and Concepts Expendable Launch Vehicles
Oriole
Terrier Orion
actual production of the rocket performed by
Nammo AS. The HTR uses liquid oxygen and rub-
berized HTPB as fuel, has a 31,000-newton (7,000-
pound-force) thrust, and a burn time of 30 to 35
seconds. Its peak altitude is designed to be between
55 and 75 kilometers (34 and 57 miles). Lockheed
Martin-Michoud obtained an International Traffic in
Arms Regulations (ITAR) Manufacturing License
Agreement from the U.S. Government in order to
gain approval for the 17-month design and handoff
project. On May 3, 2007, the HTR flew successful-
ly from the Andøya Rocket Range in Norway.
Nammo AS considered the HTR a test vehicle only,
giving the company expertise in the development
and operation of hybrid propulsion systems.32
SpaceLoft XL – UP Aerospace, Inc.
UP Aerospace, Incorporated, headquartered in
Farmington, Connecticut, with business and engi-
neering offices in Highlands Ranch, Colorado, has
developed the SpaceLoft XL sounding rocket for
research and commercial applications. The rocket, 6
meters (20 feet) tall and 25 centimeters (10 inches)
in diameter, can carry up to 50 kilograms (110
pounds) of payload to an altitude of 225 kilometers
(140 miles). A smaller version, the SpaceLoft, can
carry 9 kilograms (20 pounds) to an altitude of 130
kilometers (80 miles). UP Aerospace is marketing
the SpaceLoft family of vehicles to serve educa-
tional and research markets, such as microgravity
and atmospheric sciences experiments, as well as
commercial applications, including product market-
ing and novelty promotion.
The first successful SpaceLoft XL launch
took place on April 28, 2007, from Spaceport
America in New Mexico.33 The rocket reached a
peak altitude of 117.5 kilometers (72.7 miles), land-
ing in a mountainous region of the approved land-
ing zone at White Sands Missile Range, New
Mexico. The rocket carried over 50 student experi-
ments as well as commercial payloads from several
companies.34
20 Federal Aviation Administration Office of Commercial Space Transportation
Expendable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
Spaceloft XL
This section describes active and emerging RLV
programs in the United States. Emphasis is placed
on vehicles developed by private companies with-
out the assistance of the government. Many of these
companies are developing space hardware for the
first time. Government RLV programs are also
included to provide context, particularly since the
Space Shuttle is considered a first-generation RLV.
Experiences gained by operating the Space Shuttle
for more than 20 years have helped solve, as well
as highlight, crucial problems related to the design
of efficient RLV systems. The first subsection
addresses commercial RLV projects underway or in
development. The second subsection features gov-
ernment RLV efforts.
Commercial RLV Development Efforts
Tiger & Cardinal – Acuity Technologies
Acuity Technologies of Menlo Park,
California, has been developing the Tiger and
Cardinal vehicles to compete in the two levels of
the Northrop Grumman Lunar Lander Challenge
competition. Both vehicles are vertical takeoff and
vertical landing designs powered by isopropyl alco-
hol and 59-percent con-
centration hydrogen per-
oxide. The vehicles are
designed to maneuver
autonomously and can
also be controlled from
the ground via a stan-
dard remote control air-
craft radio link. Neither
vehicle was ready to
enter the 2007 competi-
tion but may participate
in future competitions.35
MOD – Armadillo Aerospace
Armadillo Aerospace, a former competitor for
the Ansari X Prize, is developing a family of vehi-
cles designed for suborbital and, eventually, orbital
flight opportunities. In 2007, Armadillo developed
the MOD-1 vehicle, a variant of the Quad vehicle
Armadillo built in 2006 to compete for the Northrop
Grumman Lunar Lander Challenge. The MOD-1
consists of a single pair of propellant tanks (the
Quad design featured two pairs of tanks) above a
LOX/ethanol engine, with payload and electronic
boxes on top of the tanks. The vertical-takeoff, ver-
tical-landing vehicle is supported by four large
landing legs.
Armadillo received an experimental permit
for MOD-1 in 2007 and performed flights of the
vehicle under that permit during the year. On
October 20, MOD-1 performed a low-level flight
test at the Oklahoma Spaceport to demonstrate it
was capable of performing the flight profile needed
to win Level One of the Lunar Lander Challenge.
MOD-1 then made four flights at Holloman Air
Force Base, New Mexico, during the 2007 X
PRIZE Cup in an effort to win the competition. The
vehicle successfully flew the first leg of the Level
One challenge on the afternoon of October 27, but
during the return leg suffered a “hard start” of its
engine; the engine shut down with about seven sec-
onds remaining in the flight as it hovered over the
landing pad. On the morning of October 28,
Armadillo made another attempt to win the prize
with the MOD-1, flying the initial leg of the flight
profile successfully. On the return trip, however, the
engine suffered another hard start and made a pow-
ered abort several seconds after ignition. A final
attempt to win the prize on the afternoon of
Federal Aviation Administration Office of Commercial Space Transportation 21
2008 U.S. Commercial Space Transportation Developments and Concepts Reusable Launch Vehicles
Reusable Launch Vehicles
VVeehhiiccllee:: Tiger & Cardinal
DDeevveellooppeerr:: Acuity Technologies
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 25 kg (55 lb) to 50 m (165 ft)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Lunar Lander Challenge competition
VVeehhiiccllee:: MOD
DDeevveellooppeerr:: Armadillo Aerospace
FFiirrsstt LLaauunncchh:: 2007
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 25 kg (55 lb) to 50 m (165 ft)
LLaauunncchh SSiittee:: Oklahoma Spaceport, Holloman Air ForceBase
TTaarrggeetteedd MMaarrkkeett:: Lunar Lander Challenge competition,future suborbital and orbital launch applications
Tiger and Cardinal
October 28 failed when the engine suffered another
hard start, blowing off the engine chamber and
starting a fire before the vehicle could lift off.36
After diagnosing and resolving these engine
problems, Armadillo plans to continue development
of the MOD-1, using it as the basis for a series of
increasingly-powerful modular vehicles. Future
plans call for testing vehicles that use two or more
MOD-1 vehicles in combination. A “six-pack” vari-
ant using six modules would be capable of carrying
a payload on a suborbital trajectory to 100 kilome-
ters (62 miles) altitude and could begin flight tests
in 2008. Even larger vehicles, using dozens of iden-
tical modules, could be used to launch small pay-
loads into orbit.37
BSC Spaceship – Benson Space Company
Benson Space Company (BSC), of Poway,
California, was established by former SpaceDev
CEO Jim Benson in September 2006 to develop
and operate vehicles to serve the suborbital space
tourism market. BSC originally planned to operate
a suborbital version of the Dream Chaser spacecraft
proposed by SpaceDev. However, in May 2007,
BSC unveiled a new vehicle concept, the BSC
Spaceship. The vehicle is an amalgam of several
previous NASA and
USAF aircraft and rock-
etplanes, including the
X-2, X-15, and T-38. The
BSC Spaceship will take
off vertically using
hybrid motors; after
reaching a peak altitude
of at least 105 kilometers (65 miles), the vehicle
will perform a low-g “carefree” reentry—using an
approach called variable ballistic coefficient slow-
ing—and land on a runway. BSC believes the BSC
Spaceship will be faster and less expensive to con-
struct than previous designs, allowing it to enter
commercial service as early as 2009.38
New Shepard – Blue Origin
Blue Origin is developing the New Shepard
Reusable Launch System, a suborbital, vertical-
takeoff, vertical-landing RLV for commercial pas-
senger spaceflights. The vehicle will consist of a
crew capsule, capable of carrying three or more
people, mounted on top of a propulsion module.
22 Federal Aviation Administration Office of Commercial Space Transportation
Reusable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
VVeehhiiccllee:: New Shepard
DDeevveellooppeerr:: Blue Origin
FFiirrsstt LLaauunncchh:: no later than 2010
NNuummbbeerr ooff SSttaaggeess:: 1-2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 3 people to 100 km (62 mi)
LLaauunncchh SSiittee:: Culberson County, Texas
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourism
MOD-1 on the pad at the 2007 X PRIZE Cup
VVeehhiiccllee:: BSC Spaceship
DDeevveellooppeerr:: Benson Space Company
FFiirrsstt LLaauunncchh:: 2009
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 6 people to at least 105 km (65 mi)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourism
BSC Spaceship
Blue Origin's Goddard prototype vehicle
Engines using high-test peroxide (HTP) and
kerosene will power the vehicle. The flights would
take place from a private facility operated by Blue
Origin in Culberson County, Texas.
As part of the New Shepard development
process, Blue Origin plans to build several proto-
type vehicles, which will be tested and flown from
their Texas facility. The first such vehicle, named
Goddard, is powered by an HTP monopropellant
engine and is intended to perform flights to alti-
tudes of about 600 meters (2,000 feet) and lasting
no longer than 1 minute. In September 2006, the
FAA granted Blue Origin an experimental permit to
perform those flight tests. The first permitted flight
took place on November 13, 2006, followed by
flights on March 22 and April 19, 2007.
Sea Star – Interorbital Systems
Interorbital Systems of Mojave, California, is
developing the Sea Star for microsatellite payloads
weighing up to 26 kilograms (58 pounds) and as a
testbed for its larger Neptune orbital launch vehicle.
These vehicles are constructed for design simplici-
ty. The vehicle consists of a booster module with
four rocket engines, a sustainer module with four
additional engines as well as propellant tanks and
guidance control systems, and a satellite module
that contains the payload and one small rocket
engine. All the engines use a combination of stor-
able hypergolic propellants: white fuming nitric
acid (WFNA) and “hydrocarbon X” (HX), a com-
pany-proprietary fuel. The main structures of the
rocket, including the outer shell and propellant
tanks, will use carbon composite materials. Sea Star
does not require land-based launch infrastructure.
Taking advantage of design elements derived from
submarine-launched ballistic missiles, this vehicle
will float in seawater and launch directly from the
ocean. Initial test launches of the vehicle are
planned for the second quarter of 2008.39
Neptune – Interorbital Systems
Neptune is a scaled-up version of Interorbital
Systems’ Sea Star rocket and is intended to carry
passengers into orbit. The Neptune uses a design
similar to the Sea Star vehicle, with a booster mod-
ule that has four high-thrust rocket engines and a
sustainer module with four medium-thrust engines.
The vehicle can place 3,175 kilograms (7,000
pounds) into a 51-degree, 400-kilometer (250-mile)
orbit.
A unique aspect of the
Neptune is that the main rocket
structure, once in orbit, can act as
a small space station. A conical
crew module attached to the top
of the rocket, carrying up to five
people, would undock, turn 180
degrees, and dock nose-first with
the orbital station module. The
tanks of the module, spheres 6
meters (20 feet) in diameter,
would be purged of any remain-
ing propellant, then pressurized
to serve as habitation modules.
The company has built a full-
sized, six-person crew module
5.2 meters (17 feet) in diameter
and outfitted it for crew and passenger training at
its Mojave, California, facility.40
Federal Aviation Administration Office of Commercial Space Transportation 23
2008 U.S. Commercial Space Transportation Developments and Concepts Reusable Launch Vehicles
VVeehhiiccllee:: Sea Star
DDeevveellooppeerr:: Interorbital Systems
FFiirrsstt LLaauunncchh:: 2nd quarter 2008
NNuummbbeerr ooff SSttaaggeess:: 2.5
PPaayyllooaadd PPeerrffoorrmmaannccee:: 26 kg (58 lb) to LEO
LLaauunncchh SSiittee:: Pacific Ocean west of Long Beach,California
TTaarrggeetteedd MMaarrkkeett:: Microsatellite launches
VVeehhiiccllee:: Neptune
DDeevveellooppeerr:: Interorbital Systems
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1.5
PPaayyllooaadd PPeerrffoorrmmaannccee:: 3,175 kg (7,000 lb) to LEO
LLaauunncchh SSiittee:: Pacific Ocean west of Long Beach,California
TTaarrggeetteedd MMaarrkkeett:: Orbital space tourism
Sea Star
Neptune
XA 1.0 – Masten Space Systems
Masten Space Systems of Mojave, California,
is developing the eXtreme Altitude (XA) series of
suborbital RLVs, initially designed to carry small
research payloads. The first in the series, the XA
1.0, is a vertical-takeoff, vertical-landing vehicle
powered by LOX and isopropyl alcohol engines.
The XA 1.0 is designed to carry a 100-kilogram
(220-pound) payload to an altitude of at least 100
kilometers (62 miles), performing several such
flights per day at a cost per flight of $20,000 to
$30,000. The company is selling payload space on
the vehicle for as little as $99 for a 350-gram (12-
ounce) “CanSat.” Beyond the XA 1.0, the company
has proposed the XA 1.5, which could carry a 200-
kilogram (440-pound) payload to 500 kilometers
(310 miles), and the XA 2.0, which would be able
to carry 2,000 kilograms (4,400 pounds) or five
people to 500 kilometers.
As part of the development of the XA 1.0,
Masten is building several prototype vehicles. The
first, the XA 0.1, began tethered flight tests in
2007; the vehicle was destroyed during one such
test flight in December 2007.41 A larger prototype,
the XA 0.2, is currently under development, with
plans to fly the vehicle in the 2008 Lunar Lander
Challenge.
Crusader LL – Micro-Space
Micro-Space of Denver, Colorado, is develop-
ing the Crusader LL vehicle to compete the
Northrop Grumman Lunar Lander Challenge com-
petition. The vehicle is a
vertical takeoff and verti-
cal landing design pow-
ered by a set of engines
using methyl alcohol and
hydrogen peroxide. The
modular design allows
for scaled-up vehicle
designs capable of subor-
bital spaceflight and
actual lunar lander vehicles. While Micro-Space
was not able to compete in the 2007 competition,
the company is preparing to participate in future
events.42
Crusader HTS – Micro-Space
Micro-Space of Denver, Colorado, is develop-
ing the Crusader HTS vehicle to compete the
Google Lunar X PRIZE competition as well as for
human transportation uses. This vehicle is a vertical
takeoff and vertical landing design powered by a
set of engines using methyl alcohol and hydrogen
peroxide. This high mass ratio system, coupled with
the higher performance of rocket motors in vacu-
um, will permit the vehicle not only to compete in
Level 2 of the Northrop Grumman Lunar Lander
Challenge but also to actually land a spacesuit-clad
24 Federal Aviation Administration Office of Commercial Space Transportation
Reusable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
VVeehhiiccllee:: XA 1.0
DDeevveellooppeerr:: Masten Space Systems
FFiirrsstt LLaauunncchh:: 2008
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 100 kg (220 lb) to 100 km (62 mi)
LLaauunncchh SSiittee:: Mojave Air and Space Port
TTaarrggeetteedd MMaarrkkeett:: Suborbital research payloads
XA 1.0
VVeehhiiccllee:: Crusader LL
DDeevveellooppeerr:: Micro-Space
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 25 kg (55 lb) to 50 m (165 ft)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Lunar Lander Challenge competition
VVeehhiiccllee:: Crusader HTS
DDeevveellooppeerr:: Micro-Space
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 120 kg (265 lb) to 50 km (31 mi)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Space diving, human lunar landing,Google Lunar X PRIZE
Crusader LL
astronaut on the Moon. This design positions a
standing human between two clusters of fuel tanks.
A compact rover will be substituted for the Google
Lunar X PRIZE competition. Parachute-fitted users
can easily dive from the launch vehicle at a wide
range of altitudes above the Earth. The lunar appli-
cations assume commercial launch services to lift
the landers, payload, and transstage to orbit. Micro-
Space has also developed a range of short and long
term life support systems for lightweight human
spaceflight.43
Volkon – Paragon Labs
Paragon Labs, of Denver, Colorado, is build-
ing the Volkon vehicle to compete in the Northrop
Grumman Lunar Lander Challenge. The vehicle is
a vertical takeoff, vertical landing vehicle powered
by an engine using liquid oxygen and E85 ethanol,
the first known use of E85 in a bipropellant rocket
engine. Volkon was not ready to compete in the
2007 competition, but Paragon Labs plans to con-
tinue development of the vehicle in order to partici-
pate in future competitions.44
Silver Dart – PlanetSpace
PlanetSpace, headquartered in Chicago,
Illinois, is developing the Silver Dart reusable
spacecraft for missions
to LEO. The Silver Dart
is based on the FDL-7
hypersonic glider design
originally proposed by
the U.S. Air Force Flight
Dynamics Laboratory in
the late 1950s. The vehi-
cle design features an all
metal thermal protection
system to enable flight in all weather conditions.
The Silver Dart has a glide range of 40,000 kilome-
ters (25,000 miles), or one orbit of the Earth, and a
cross range of over 6,400 kilometers (4,000 miles),
allowing the vehicle to leave LEO at any time and
still land in the continental U.S. PlanetSpace pro-
posed to launch the Silver Dart with an expendable
rocket called Nova, also under development, from a
proposed spaceport in Cape Breton, Nova Scotia.45
Rocketplane XP – Rocketplane Global
Rocketplane Global, a subsidiary of
Rocketplane Inc. of Oklahoma City, Oklahoma, is
developing the Rocketplane XP suborbital RLV.
The vehicle will take off under jet power. At an alti-
tude of at least 12,200 meters (40,000 feet), it will
ignite a single AR-36 rocket LOX and kerosene
rocket engine provided by Polaris Propulsion for a
Federal Aviation Administration Office of Commercial Space Transportation 25
2008 U.S. Commercial Space Transportation Developments and Concepts Reusable Launch Vehicles
VVeehhiiccllee:: Rocketplane XP
DDeevveellooppeerr:: Rocketplane Global
FFiirrsstt LLaauunncchh:: 2010
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 6 people to 100 km (62 mi)
LLaauunncchh SSiitteess:: Oklahoma Spaceport
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourism, microgravityresearch
VVeehhiiccllee:: Volkon
DDeevveellooppeerr:: Paragon Labs
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 25 kg (55 lb) to 50 m (165 ft)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Lunar Lander Challenge competition
Volkon
VVeehhiiccllee:: Silver Dart
DDeevveellooppeerr:: PlanetSpace
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 3
PPaayyllooaadd PPeerrffoorrmmaannccee:: TBD
LLaauunncchh SSiittee:: Cape Breton Space Port, Nova Scotia,Canada
TTaarrggeetteedd MMaarrkkeett:: Passenger and cargo missions to LEO
Silver Dart
70-second burn. The Rocketplane XP will fly to an
altitude of at least 100 kilometers (62 miles) before
reentering and landing, either under jet power or
unpowered, at the same site as takeoff.
In October 2007, Rocketplane Global
unveiled a new design for the Rocketplane XP. The
previous design, based on a highly-modified Learjet
fuselage, was replaced with a larger cabin capable
of carrying one pilot and five passengers. The jet
engines were upgraded to the more powerful J-85
version. The V-tail of the previous design has been
replaced with a T-tail, and the landing gear with a
model based on the gear used for the F-5 aircraft.
Rocketplane Global estimates that over 200,000
person-hours went into developing the new design.
The company anticipates beginning flight tests in
2010, contingent on raising sufficient capital to
fund vehicle development.46
K-1 – Rocketplane Kistler
Rocketplane Kistler (RpK), a subsidiary of
Rocketplane Inc. of Oklahoma City, Oklahoma, is
developing the K-1 orbital RLV. The K-1, whose
design dates back to the mid-1990s, is a two-stage
RLV capable of placing up to 5,700 kilograms
(12,500 pounds) into LEO. Originally developed
primarily to launch satellites into LEO and other
orbits, the K-1 is now being developed to serve the
ISS cargo and crew resupply market as well as
satellite launch and other applications.
The first stage of the K-1, called the Launch
Assist Platform (LAP), is powered by three
LOX/kerosene GenCorp Aerojet AJ26-58/-59
engines, capable of generating 4.54 million newtons
(1.02 million pounds-force) of thrust. After launch,
the LAP separates from the second stage and
restarts its center engine to put the stage on a return
trajectory to a landing area near the launch site,
using parachutes and air bags. The second stage,
called the Orbital Vehicle (OV), continues into
LEO, powered by a single Aerojet AJ26-60 engine
with a thrust of 1.76 million newtons (395,000
pounds-force). At the end of its mission, a LOX and
ethanol thruster performs a deorbit burn. The OV
lands near the launch site using a parachute and
airbag combination similar to the LAP. Initial
flights of the K-1 are planned to take place from
Spaceport Woomera in South Australia, with later
flights staged from a U.S. site to be determined.
RpK was formed in
early 2006 with the merger
of Rocketplane Ltd. with
Kistler Aerospace
Corporation, which had been
developing the K-1 concept
since the 1990s but had sus-
pended work because of
financial problems. In August
2006, RpK was one of two
companies to receive a fund-
ed COTS award from NASA
to help develop the K-1 to
service the ISS. The compa-
ny achieved several milestones outlined in the
Space Act agreement with NASA for the COTS
program through early 2007, including a system
requirement review for the K-1.47 However, the
company failed to achieve a financial milestone of
the COTS agreement requiring it to raise several
hundred million dollars of private capital to fully
fund the development of the K-1. In October 2007,
NASA announced it had terminated the COTS
agreement with RpK after awarding the company
only $32.1 million of the original $207 million.48
26 Federal Aviation Administration Office of Commercial Space Transportation
Reusable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
K-1
Rocketplane XP
VVeehhiiccllee:: K-1
DDeevveellooppeerr:: Rocketplane Kistler
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 5,700 kg (12,500 lb) to LEO
LLaauunncchh SSiitteess:: Woomera, Australia; U.S. site TBD
TTaarrggeetteedd MMaarrkkeett:: ISS crew and cargo resupply, satellitelaunch, orbital space tourism
SpaceShipTwo –
Scaled Composites, LLC/The SpaceshipCompany/Virgin Galactic
Scaled Composites, LLC, and Virgin Galactic,
LLC a subsidiary of the Virgin Group of
Companies, announced the formation of a joint
venture, called The Spaceship Company (TSC),
LLC, in July 2005. The purpose of TSC is to over-
see development and production of SpaceShipTwo,
a commercial suborbital spacecraft based on tech-
nology developed for SpaceShipOne. TSC will pro-
duce the first five SpaceShipTwo vehicles for
Virgin Galactic, which plans to put them into com-
mercial service once test flights are completed,
offering suborbital space flights for private individ-
uals, science research, and payload. The venture
will also develop a carrier aircraft,
WhiteKnightTwo, that will be used to air-launch
SpaceShipTwo in much the same manner that the
original White Knight aircraft air-launched
SpaceShipOne.
During 2007, Virgin Galactic’s first 100 cus-
tomers were invited to undertake g-force training at
the NASTAR training center outside Philadelphia.
The resulting unique dataset is now being used by
the company as it develops its policies for future
customer training and safety.
In January 2008, Virgin Galactic and Scaled
Composites unveiled the designs for WhiteKnightTwo
and SpaceShipTwo before the start of the test flight
program for both vehicles scheduled for 2008.49
Dream Chaser – SpaceDev
Dream Chaser is an RLV under development
by SpaceDev to serve suborbital and orbital appli-
cations. The design of this vehicle is based on the
NASA HL-20 spaceplane concept from the early
1990s, which was itself inspired by the successfully
launched Soviet BOR-4 spaceplane from the early
1980s. Dream Chaser
has been expanded from
the original HL-20 by
10% to an overall length
of 9.6 meters (31.5 feet)
and wingspan of 8
meters (26.2 feet). The
Dream Chaser is capable of transporting 6-9 pas-
sengers, compared to the original HL-20’s capacity
of 6-10. For suborbital flights, the vehicle will
launch vertically, using hybrid engines. On orbital
flights, the vehicle will launch on top of existing
launch vehicles. In both scenarios, the vehicle will
glide to a runway landing.
The Dream Chaser concept was one of the
finalists in the original round of NASA’s COTS
competition, and was resubmitted as a bid for the
COTS-2 competition. In June 2007, NASA and
SpaceDev signed an unfunded Space Act agreement
(SAA) where NASA will provide technical support
and other information to SpaceDev to aid in the
Federal Aviation Administration Office of Commercial Space Transportation 27
2008 U.S. Commercial Space Transportation Developments and Concepts Reusable Launch Vehicles
SpaceShipTwo
VVeehhiiccllee:: SpaceShipTwo
DDeevveellooppeerr:: Scaled Composites
FFiirrsstt LLaauunncchh:: 2010
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 8 people to minimum of 100 km(62 mi)
LLaauunncchh SSiitteess:: Mojave Air and Space Port, SpaceportAmerica
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourismVVeehhiiccllee:: Dream Chaser
DDeevveellooppeerr:: SpaceDev
FFiirrsstt LLaauunncchh:: 4th quarter 2009 (suborbital), 2nd quar-ter 2011 (orbital)
NNuummbbeerr ooff SSttaaggeess:: 2 (suborbital), 3 (orbital)
PPaayyllooaadd PPeerrffoorrmmaannccee:: 6-9 people
LLaauunncchh SSiittee:: Spaceport America (suborbital), CCAFS(orbital)
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourism, ISS crewand cargo resupply, orbital space tourism, military mis-sions
Dream Chaser
ongoing development of Dream Chaser.50 SpaceDev
has completed two technical milestones to date
under the unfunded SAA. In addition, SpaceDev
signed a memorandum of understanding with ULA
in April 2007 to study the use of the Atlas 5 to
launch Dream Chaser on orbital missions.51
SpaceDev is also working with ATK to study the
integration of the Dream Chaser on an Ares 1-
derived launch vehicle.
Skyhopper – Space Access, LLC
In December 2007, Space Access, LLC, of
Huntertown, Indiana, announced its plans to devel-
op a suborbital RLV called Skyhopper. The vehicle
would take off and land on a conventional runway,
and use ejector ramjet engines with liquid hydrogen
fuel, as opposed to conventional rocket engines.
Space Access anticipates Skyhopper will reach
speeds of up to Mach 7 and altitudes in excess of
100 kilometers (62 miles). The company plans on
building up to eight Skyhopper vehicles and operate
up to 15 flights per day. Suborbital flight operations
are scheduled to begin in 2011, initially from a
facility to be developed south of Corpus Christi,
Texas. Orbital flights, using a variant of Skyhopper,
are projected to begin as soon as 2014.52
Falcon 1 – Space Exploration Technologies Corporation
SpaceX of Hawthorne, California, has devel-
oped the partially reusable Falcon 1 launch vehicle,
that can place up to 475 kilograms (1,050 pounds)
into LEO for about $7 million. The first stage of
this vehicle is designed to parachute into the ocean.
It can then be recovered, refurbished, and reused.
SpaceX privately developed the entire two-stage
vehicle from the ground up, including the engines,
cryogenic tank structure, and guidance system. The
first stage engine, known as
Merlin, uses pump-driven
LOX and kerosene. The sec-
ond stage engine, called
Kestrel, uses a pressure-fed
LOX and kerosene system.
The Falcon 1e, an enhanced
version of the Falcon 1 with
a stretched first stage and
larger payload fairing, is
slated to enter service in
2009; it will be able to place
up to 725 kilograms (1,600
pounds) into LEO for $8.5
million.53
The second Falcon 1 launch, designated
Demo Flight 2, took place on March 20, 2007, from
Omelek Island in the Kwajalein Atoll in the Pacific
Ocean. The vehicle failed to reach orbit because of
an upper stage control anomaly that coupled with
slosh in the stage’s LOX tank. This caused a rolling
motion that centrifuged the propellants away from
the tank outlets and caused the engine to shut down
prematurely. SpaceX has taken several steps to
resolve the problem, including installing slosh baf-
fles in the second stage LOX tank.54 Falcon 1 will
return to flight in early 2008, carrying a number of
small payloads, to be followed by the first Falcon 1
commercial launch, of the Malaysian remote sens-
ing spacecraft Razaksat.
28 Federal Aviation Administration Office of Commercial Space Transportation
Reusable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
VVeehhiiccllee:: Falcon 1
DDeevveellooppeerr:: Space Exploration Technologies Corporation
FFiirrsstt LLaauunncchh:: 2006
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: 475 kg (1,050 lb) to LEO
LLaauunncchh SSiittee:: Kwajalein Atoll, VAFB
TTaarrggeetteedd MMaarrkkeett:: Small satellite launch
VVeehhiiccllee:: Skyhopper
DDeevveellooppeerr:: Space Access, LLC
FFiirrsstt LLaauunncchh:: 2011
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: TBD
LLaauunncchh SSiittee:: Near Corpus Christi, Texas
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourism
Skyhopper
Falcon 1
Falcon 9 –Space Exploration Technologies Corporation
The Falcon 9 vehicle is a two-stage RLV
designed to launch large spacecraft as well as cargo
and crew resupply missions to the ISS. The first
stage uses nine Merlin 1C engines, the same engine
as used on the first stage of the Falcon 1. The sec-
ond stage, a shortened version of the first stage,
uses a single Merlin engine. Both
stages are designed to be recovered
and reused. The Falcon 9 can place
up to 9,900 kilograms (21,820
pounds) into LEO and 4,900 kilo-
grams (10,800 pounds) into GTO. A
variant, the Falcon 9 Heavy, uses
two additional first stages as strap-
on boosters, like the Delta IV
Heavy, and can place up to 27,500
kilograms (60,600 pounds) into
LEO and 12,000 kilograms (26,500
pounds) into GTO.55 Launch costs
range from $35 million for the
medium version to $90 million for
the heavy version, in 2007 dollars.56
The first Falcon 9 launch, a demonstration
mission, is scheduled for the fourth quarter of 2008.
SpaceX will perform three launches in 2008 and
2009 as part of its COTS agreement with NASA;
other Falcon 9 customers include MacDonald,
Dettwiler and Associates Ltd. of Canada, Bigelow
Aerospace, and Avanti Communications, which
signed the first contract for the Falcon 9 launch of a
commercial communications satellite in September
2007.57 In November 2007, SpaceX broke ground
on new launch facilities for the Falcon 9 at Space
Launch Complex 40, a former Titan 4 launch pad at
CCAFS. The facility will be ready to support the
first Falcon 9 launch in late 2008.58
In August 2006, SpaceX won a COTS demon-
stration award from NASA with a maximum value
of $278 million. Under terms of the award, SpaceX
will perform three Falcon 9 launches of its Dragon
reusable spacecraft in late 2008 and early 2009 to
demonstrate its ability to ferry cargo to and from
the ISS.
Laramie Rose – SpeedUp
SpeedUp of Laramie, Wyoming, is developing
the Laramie Rose vehicle to compete in the
Northrop Grumman Lunar Lander Challenge com-
petition. The vehicle, being built in partnership with
Frontier Astronautics of Chugwater, Wyoming, is a
vertical takeoff and vertical landing design powered
by an engine using 90-percent concentration hydro-
gen peroxide. The vehicle is also designed to be a
technology testbed for future rocket-powered recre-
ational vehicles planned by the company. While
Laramie Rose was not able to compete at the 2007
competition, the vehicle
hardware is 99-percent
complete and SpeedUp
has performed static
engine tests, and the
company plans to com-
pete in the 2008 compe-
tition.59
Michelle-B – TGV Rockets, Inc.
TGV Rockets, Inc. (TGV) is developing
Michelle-B, a fully reusable, remotely-piloted sub-
Federal Aviation Administration Office of Commercial Space Transportation 29
2008 U.S. Commercial Space Transportation Developments and Concepts Reusable Launch Vehicles
VVeehhiiccllee:: Falcon 9
DDeevveellooppeerr:: Space Exploration Technologies Corporation
FFiirrsstt LLaauunncchh:: 2008
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: Up to 27,500 kg (60,600 lb) toLEO, 12,000 kg (26,500 lb) to GTO
LLaauunncchh SSiittee:: Kwajalein Atoll, VAFB
TTaarrggeetteedd MMaarrkkeett:: Launch of medium and large satellites, ISS crew and cargo resupply
VVeehhiiccllee:: Michelle-B
DDeevveellooppeerr:: TGV Rockets
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 1,000 kg (2,200 lb) to 100 km(62 mi)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Remote sensing, science, includingmicrogravity research; national security applications
Falcon 9
VVeehhiiccllee:: Laramie Rose
DDeevveellooppeerr:: SpeedUp
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 25 kg (55 lb) to 50 m (165 ft)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Lunar Lander Challenge competition
Laramie Rose
orbital vehicle, designed
to carry up to 1,000 kilo-
grams (2,200 pounds) to
an altitude of 100 kilo-
meters (62 miles). This
vehicle uses a vertical
take-off and landing
design, with a drag
shield to assist in deceleration during landing.
Michelle-B will provide up to 200 seconds of
microgravity, while not exceeding 4.5 g during any
phase of flight. Using existing optical packages, the
vehicle can provide 60-centimeter oblique imagery.
Six pressure-fed LOX and kerosene engines for use
on ascent and landing power the vehicle. TGV’s
design is intended to enable high reusability,
require minimal ground support, and allow the
vehicle to return to flight within a few hours of
landing. The company has completed a preliminary
design review of the Michelle-B and, in the second
quarter of 2007, performed a test of their “work-
horse” engine for the vehicle. The company is now
working to complete a prototype engine based on
the lessons learned from those tests.60
Crew Transfer Vehicle –Transformational Space LLC
Transformational Space (t/Space) LLC, of
Reston, Virginia, has proposed developing the Crew
Transfer Vehicle (CXV) reusable spacecraft, capa-
ble of carrying several people to the ISS or other
destinations in low Earth orbit. The CXV would be
air-launched by a scaled-up version of the
QuickReach ELV being developed by AirLaunch
LLC. The capsule design is derived from that
developed for the Discoverer/Corona program near-
ly 50 years ago, and permits a safe reentry regard-
less of initial orientation even if the capsule’s con-
trol systems fail. The CXV is designed to land in
water and be reused after a nominal refurbish-
ment.61
T/Space proposed the CXV during the initial
COTS competition in 2006, but was not selected
for a funded Space Act agreement. The company
did sign an unfunded Space Act agreement with
NASA in February 2007 to guide continued devel-
opment of the CXV. T/Space submitted a proposal
for the new COTS competition in November 2007.
Burning Splinter – Unreasonable Rocket
Unreasonable Rocket of Solana Beach,
California, is a father-son team developing the
Burning Splinter vehicle to compete in the
Northrop Grumman Lunar Lander Challenge. The
vertical takeoff, vertical landing vehicle is powered
by four engines using liquid oxygen and ethanol
propellants. The team completed the vehicle hard-
ware and performed some engine test firings, but
was not able to get the
vehicle ready to fly in
time for the 2007 com-
petition. Unreasonable
Rocket is planning some
modifications to the
design to improve its
performance for future
competitions.62
Reusable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
30 Federal Aviation Administration Office of Commercial Space Transportation
Michelle B
VVeehhiiccllee:: Crew Transfer Vehicle (CXV)
DDeevveellooppeerr:: Transformational Space LLC
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 2
PPaayyllooaadd PPeerrffoorrmmaannccee:: Three people or 910 kg (2000 lb)to LEO
LLaauunncchh SSiittee:: TBD (air launched)
TTaarrggeetteedd MMaarrkkeett:: Crew and cargo to the ISS, orbitalspace tourism
CXV
VVeehhiiccllee:: Burning Splinter
DDeevveellooppeerr:: Unreasonable Rocket
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 25 kg (55 lb) to 50 m (165 ft)
LLaauunncchh SSiittee:: TBD
TTaarrggeetteedd MMaarrkkeett:: Lunar Lander Challenge competition
Burning Splinter
Xerus – XCOR Aerospace
In July 2002, XCOR Aerospace announced
plans to develop a suborbital RLV, named Xerus.
The Xerus would take off horizontally from a run-
way under rocket power and fly to an altitude of
100 kilometers (62 miles) before returning for a
runway landing. XCOR plans to use Xerus for a
variety of suborbital missions, including micrograv-
ity research, suborbital
tourism, and even the
launch of very small
satellites into orbit.
Xerus is expected to
have the ability to launch
a 10-kilogram (22-
pound) payload to LEO.
In April 2004, XCOR Aerospace received a
license from the FAA to perform flights of an inter-
mediate demonstration vehicle, called Sphinx, from
Mojave Air and Space Port. That license expired at
the end of 2006 with no flights having taken place.
XCOR continues fundraising and technical devel-
opment for the vehicle and anticipates filing a new
license application for it when ready.
Government RLV Development Efforts
Throughout the 1980s and 1990s, the DoD
and NASA conducted several joint and independent
programs to produce experimental RLVs. These
vehicles were intended to improve reliability, mini-
mize operating costs, and demonstrate “aircraft-
like” operations. However, none of these concepts
resulted in a fully operational vehicle. In recent
years, these technology development efforts dimin-
ished. The U.S. Department of Defense focused on
operating its large EELV vehicles and developing
small responsive launch vehicles, although it is
devoting some resources to technology develop-
ment that is relevant to RLVs. NASA has shifted its
emphasis to developing large ELVs designed to
implement the Vision for Space Exploration.
Space Shuttle
Consisting of an expendable external tank,
two reusable solid rocket boosters, and a reusable
Orbiter, NASA’s STS (Space Transportation
System), commonly referred to as the Space
Shuttle, has conducted 120 launches since its intro-
duction in 1981.
The three
remaining orbiters—
Atlantis, Discovery,
and Endeavour—
returned to flight in
July 2005 after the
loss of Columbia in
February 2003.
Today, the Space
Shuttle is the only
available means for
completing assem-
bly of the ISS.
Intending to use the
Shuttle until 2010,
NASA is committed
to investing in the
Space Shuttle fleet
to maintain safety
and reliability and
extend orbiter service life until its role in construct-
ing the ISS is complete. Thirteen Space Shuttle
flights, including one mission to service the Hubble
Space Telescope, are planned before the fleet is
retired in 2010. The Space Shuttle’s day-to-day
operations are managed by United Space Alliance,
a Boeing-Lockheed Martin joint venture in opera-
tion since 1996.
2008 U.S. Commercial Space Transportation Developments and Concepts Reusable Launch Vehicles
Federal Aviation Administration Office of Commercial Space Transportation 31
VVeehhiiccllee:: Xerus
DDeevveellooppeerr:: XCOR Aerospace
FFiirrsstt LLaauunncchh:: TBD
NNuummbbeerr ooff SSttaaggeess:: 1
PPaayyllooaadd PPeerrffoorrmmaannccee:: 10 kg (22 lb) to LEO
LLaauunncchh SSiittee:: Mojave Air and Space Port
TTaarrggeetteedd MMaarrkkeett:: Suborbital space tourism, nanosatel-lite launch, microgravity research
Space Shuttle
Xerus
VVeehhiicclleess:: Atlantis, Discovery, and Endeavour
DDeevveellooppeerr:: Rockwell International (now Boeing); fleet ismanaged, operated, and maintained on the ground byUnited Space Alliance, a joint venture between Boeingand Lockheed Martin
FFiirrsstt LLaauunncchh:: 1981
NNuummbbeerr ooff SSttaaggeess:: 1.5
PPaayyllooaadd PPeerrffoorrmmaannccee:: 24,900 kg (54,890 lb) to LEO
LLaauunncchh SSiittee:: KSC
MMaarrkkeettss SSeerrvveedd:: Non-commercial payloads, ISS access
Fully-Reusable Access to Space TechnologyProgram
The Fully-Reusable Access to Space
Technology (FAST) program is an effort by AFRL
to develop technologies for use in RLVs capable of
“aircraft-like” operations. FAST calls for the
methodical development of these key technologies
initially through ground experiments and later in
flight tests, with the ultimate goal of flying a
ground-launched suborbital vehicle capable of fly-
ing to speeds of Mach 4-7, as well as being capable
of reentering at Mach 25 if launched as the upper
stage of another vehicle. This experimental vehicle
could be later scaled up to larger, operational vehi-
cles. Current plans call for ground-based technolo-
gy tests to continue through 2011, with first flights
of the experimental suborbital vehicle slated for
2013.63
AFRL has issued contracts with several com-
panies to work on elements of the FAST program.
In March 2007, AFRL awarded Andrews Space a
contract to develop the program requirements for a
series of technology experiments that will be part of
the overall effort.64 In November 2007, Lockheed
Martin Michoud Operations won a $14 million con-
tract to work on airframe technologies, including
composite structures and thermal protection sys-
tems, as a part of the FAST program.65 In December
2007, AFRL awarded Northrop Grumman a 39-
month, $5.2-million contract to study responsive
ground operations and perform experiments and
simulations to support the development of a future
operations control center.66
Reusable Launch Vehicles 2008 U.S. Commercial Space Transportation Developments and Concepts
32 Federal Aviation Administration Office of Commercial Space Transportation
A number of new orbital transportation systems are
being developed by U.S. entities. These systems
range from government reusable crewed and cargo
vehicles to commercial habitats. These develop-
ments will provide critical manned and unmanned
orbital operations and transportation in the post-
Shuttle era after 2010. A number of technologies
have been demonstrated for these systems during
the past year and show progress towards planned
operational capability.
NASA has development contracts for the
civilian-use Orion crew exploration vehicle and one
active award for commercial ISS crew and cargo
demonstrations through the COTS program, with
additional awards planned. The U.S. Air Force has
plans for a military-use X-37B Orbital Transfer
Vehicle (OTV) that will carry payloads into orbit.
Finally, Bigelow Aerospace is in the process of
developing commercial orbital habitats.
Orion Crew Exploration Vehicle
The U.S. plan for space exploration calls for
continued missions to LEO and later missions to
the Moon, Mars, and beyond. To achieve LEO,
lunar, and other future missions, NASA has initiat-
ed the development of the Orion Crew Exploration
Vehicle (CEV) to carry people and pressurized
cargo into space. The spacecraft will consist of a
combined pressurized crew module and service
module that is launched into orbit by the Ares I
crew launch vehicle. The current Orion design has
the capacity to transport up to six crew members to
the ISS or four people on missions to the Moon.
The first flight of Orion carrying humans is to
occur no later than 2015, and the first flight to the
Moon is planned for no later than 2020. For mis-
sions to the Moon, an Orion capsule will ren-
dezvous with an Ares V-launched lunar landing
module and Earth departure stage in LEO to con-
duct its mission. At the end of these missions,
Orion will be the atmospheric reentry vehicle.67
The spacecraft’s conical shape is similar to
the capsules predating the Shuttle, but Orion will
contain state-of-the-art technologies provided by
the contracting team and NASA. The capsule will
reenter the atmosphere using a newly-developed
thermal protection system. Other new technologies
will include computing and electronics, a powered
system for launch abort that will sit atop the Orion
capsule (for which unmanned abort testing will
commence in 2008), and landing technology.68 In
addition, Orion’s 5-meter (16.5-foot) diameter will
allow for more than twice the volume—doubling
crew capacity and increasing interior space—of
Apollo-era modules.
Lockheed Martin is the prime contractor for
the Orion crew vehicle under NASA’s Constellation
Program and led by the Orion Project Office at
Johnson Space Center. NASA announced the prime
contractor selection on August 31, 2006, and work
has proceeded at the NASA centers and contractor
locations. NASA opted for Lockheed Martin’s
design over that of a Northrop Grumman-Boeing
team and awarded an initial seven-year base con-
tract worth just under $4 billion. The contract con-
tains an option worth another $4 billion for produc-
tion and operational engineering activity up to
2019. Lockheed Martin’s contracting team includes
Honeywell, Orbital Sciences, United Space
Alliance, and Hamilton Sundstrand. Contracts for
the lunar lander and earth departure stage have not
yet been awarded.
Every NASA center has a role in the Orion
mission. For example, Langley Research Center is
the lead for developing the launch abort system,
Glenn Research Center is leading the service mod-
ule and spacecraft adapter development, and
Marshall Space Flight Center and Kennedy Space
Center will provide the Ares launch vehicles and
Orion launch services, respectively.69
Federal Aviation Administration Office of Commercial Space Transportation 33
In-Space Technology 2008 U.S. Commercial Space Transportation Developments and Concepts
Reentry Vehicles and In-Space Technology
Orion CEV
International Space Station Crew andCargo Transport
The decision to finish constructing the ISS by
the end of the decade and maintain its operation
with a six-person crew reinforces the demand for
continual transport flights to and from the station.
Several government systems to fulfill this demand
are either operational or planned. The Shuttle will
be the primary American system for bringing new
station components, crew, and cargo to the ISS until
Shuttle retirement, after which Orion will provide
this service. Russia’s Soyuz crew and Progress
cargo vehicles are current robust international sys-
tems for replenishing the station. Additional inter-
national capacity is planned, including the Japanese
H-2 Transfer Vehicle and European Automated
Transfer Vehicle (ATV) that are both currently in
the development stage, with the first ATV planned
for launch in early 2008.
American commercial vehicles are planned to
supplement these government systems for crew and
cargo transport to the ISS in the future. On August
16, 2006, NASA announced the signing of two
funded Space Act Agreements with American com-
panies to develop and demonstrate the ability to
provide transportation services to the ISS, under the
COTS demonstration program. One of these agree-
ments, with Rocketplane Kistler (RpK), has since
been terminated for failure to meet required mile-
stones related to the development of its K-1 vehicle
planned for orbital crew and cargo transport. The
remaining company, SpaceX, has met its necessary
deadlines and is building the Falcon 9 launcher and
Dragon spacecraft to prove the necessary transport
capabilities under Phase 1 of the agreement, which
calls for three vehicle flights before 2010.
NASA is conducting a second competition for
a funded COTS Phase 1 agreement to replace the
terminaed 2006 agreement. This second competi-
tion commenced in October 2007 with a winner to
be announced in February 2008. A total of $174.7
million—the remaining funds from the original
agreement with RpK—will be made available to
any winning company of the new competition. The
COTS concepts will demonstrate a combination of
pressurized and unpressurized cargo delivery, dis-
posal, and return, as well as the option for crew
transport. Fixed payments will be made to the com-
panies as they achieve milestones for design and
development. Phase 2, a separate contracting oppor-
tunity from Phase 1, will consist of a competitive
procurement of cargo services to the ISS with an
option for crew services. In addition to the COTS
agreements, the companies plan to provide their
vehicles for other commercial and government mar-
kets.70
SpaceX Dragon
Initiated internally by SpaceX in 2005, the
Dragon spacecraft will be used for the commercial
transportation of cargo and crew to and from LEO.
As part of NASA's COTS program, SpaceX will
conduct a series of three Falcon 9 launches to send
a cargo-carrying Dragon into LEO where it will
demonstrate the ability to maneuver, dock with the
ISS, and return to Earth using a water landing. The
first test flight of Dragon is planned for the second
half of 2008, with subsequent launches over the fol-
lowing years.
The 4-meter (13-foot) diameter Dragon con-
sists of two modules: the trunk and capsule. The
unpressurized trunk module carries solar arrays,
thermal radiators, and stowage area for unpressur-
ized cargo. The capsule module consists of a nose
cone to protect the vessel and docking adaptor dur-
ing ascent, a pressurized section housing the crew
and/or pressurized cargo, and a service section sur-
rounding the base of the pressurized section and
34 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts In-Space Technology
SpaceX Dragon
containing avionics, reaction control system, para-
chutes, and other support infrastructure. The struc-
tural design of Dragon will be identical for cargo
and crew missions, providing a capacity of over
2,500 kilograms (5,500 pounds) for launch and
return in either configuration. In crew mode, the
vehicle can carry up to seven people, and will be
able to remain at the ISS for six months at a time,
providing emergency return capability for the entire
seven-person ISS crew. SpaceX has constructed
full-scale engineering models of the capsule pres-
sure vessel, heat shield, and other systems.71
Private funding for Dragon will be supple-
mented with NASA COTS funding through a Space
Act Agreement, as the company achieves vehicle
milestones. The current plan for NASA funding
includes $278 million, which could change as the
demonstration process continues. SpaceX
announced that it also submitted a proposal for the
new COTS competition in late 2007, with the inten-
tion of receiving funding for Dragon crewed capa-
bility.
Other Commercial Crew and Cargo TransportConcepts
NASA signed unfunded Space Act
Agreements with five companies to help develop
various vehicles and technologies that could lead to
orbital crew and cargo missions in the future. These
five companies, along with another that does not
have a current Agreement, have created system
development teams and submitted proposals for the
new COTS Phase 1 competition.72 These systems
are planned to provide transport to the ISS and
other orbital locations.
• Constellation Services International and
Space Systems Loral (SS/L) have proposed
a cargo system based on the SS/L LS-1300
satellite bus.
• PlanetSpace has teamed with Lockheed
Martin Space Systems, ATK, and the Bank
of Montreal to develop the Modular Cargo
Carrier.
• SpaceDev’s Dream Chaser Space
Transportation System is a lifting body
RLV that the company conceptually will
launch on an Atlas V.
• SPACEHAB is proposing its Advanced
Research and Conventional Technology
Utilization Spacecraft (ARCTUS) for
orbital transport.
• Transformational Space (t/Space) is devel
oping the CXV Crew Transfer Vehicle, a
transport and reentry vehicle based on
Discoverer and Corona capsule design.
• Andrews Space, which does not have a
current Space Act Agreement, proposed the
Andrews Cargo Module logistics system.
X-37B Orbital Test Vehicle
The U.S. Air Force Rapid Capabilities Office
is leading development of an unmanned reusable
space vehicle designated the X-37B Orbital Test
Vehicle (OTV). This new capability will serve as a
platform for science and technology demonstration
and testing. Experiments will be carried in a pay-
load bay, which can open and expose its contents to
the space environment, similar to the bay in the
Federal Aviation Administration Office of Commercial Space Transportation 35
In-Space Technology 2008 U.S. Commercial Space Transportation Developments and Concepts
Concept of X-37 vehicle, similar to X-37B in development
Concept of SpaceX’s Dragon vehicle with crew
Space Shuttle. This vehicle leverages previous work
NASA, DARPA, AFRL, and Boeing completed for
the X-37 program. As it was for the original X-37
vehicle, Boeing is the prime contractor for the
OTV.
The OTV will launch vertically into orbit on
an expendable rocket and have the ability to deorbit
on command and land horizontally for reuse. Initial
plans call for launching the first OTV from CCAFS
on an Atlas V in 2008. The vehicle will then deorbit
and land on a runway at either VAFB or EAFB in
California.73 The first flights will be used for vehi-
cle testing, after which operational technology
experiment flights will be conducted.
Commercial Orbital HabitatDevelopment
Bigelow Aerospace is developing next-gener-
ation, expandable space habitat technology that is
intended to support a future private-sector-driven
commercial space industry. The company has man-
ufactured, launched, and is operating two technolo-
gy demonstration spacecraft (Genesis I and Genesis
II) that are validating the fundamental engineering
concepts necessary to construct an expandable
orbital habitat. Bigelow Aerospace is currently
planning to construct and launch larger and more
complex spacecraft over the next few years, all of
which are being designed to support a crewed pres-
ence in LEO.
The Genesis II pathfinder spacecraft was
launched on June 28, 2007, less than one year after
the Genesis I launch on July 12, 2006. Both of
these spacecraft were successfully orbited by an
ISC Kosmotras Dnepr rocket launched from facili-
ties at the new Yasny Cosmodrome in the Orenburg
region of the Russian Federation. The two space-
craft are externally similar although internally dif-
ferent; Genesis II was outfitted with additional sen-
sors, cameras, and unique interior payloads. The
size of the demonstrators are approximately 4.4
meters (15 feet) in length and 1.6 meters (5.3 feet)
in diameter at launch, expanding to 2.54 meters (8
feet) in diameter after full deployment is achieved
in orbit. The spacecraft have a usable volume of
11.5 cubic meters (406 cubic feet) and an anticipat-
ed orbital lifespan of 3 to 13 years. Bigelow
Aerospace uses its mission control facility in North
Las Vegas, Nevada to operate these spacecraft.
Bigelow Aerospace will next continue its
habitat development with the larger Sundancer
spacecraft. The successful test and demonstration of
technologies on the two Genesis spacecraft and the
increasing cost of orbital launch has led Bigelow
Aerospace to decide to proceed directly with the
Sundancer, the company’s first attempt at producing
a habitat capable of supporting a human presence
on orbit. The planned launch date for Sundancer is
in approximately 2010. The spacecraft is currently
anticipated to weigh around 8,600 kilograms
(19,000 pounds) and offer roughly 180 cubic meters
(6,350 cubic feet) of usable volume. The technolo-
gies to be demonstrated and deployed on Sundancer
include environmental control and life support sys-
tems; guidance, navigation, and attitude control;
propulsion; power generation; and windows.
Subsequent to Sundancer, Bigelow Aerospace plans
to launch a node/bus combination that will mate
with the Sundancer to form the core of the compa-
ny’s first space complex. If this activity is success-
ful, Bigelow Aerospace would then launch a full
standard module that will also be attached to the
Sundancer and node/bus complex.
In-Space Technology 2008 U.S. Commercial Space Transportation Developments and Concepts
36 Federal Aviation Administration Office of Commercial Space Transportation
External view of Genesis II
Bigelow Aerospace has executed agreements
to explore relationships with various launch
providers including Lockheed Martin and SpaceX
for the possible use of the Atlas V or Falcon 9 vehi-
cles, respectively, for future module and crew or
cargo launches..
A critical issue for Bigelow Aerospace is the
provision of transportation services to bring people
and cargo to and from its platforms in LEO. The
company would benefit from the availability of a
low-cost and reliable commercial human-rated
transportation system that could dock with
Sundancer and future space complexes. For this
reason, the company has created two initiatives to
promote new vehicle development: the $50 million
America’s Space Prize (see the Space Prize
Competitions section) and an offer to place $100
million in escrow to begin contracting for launch
services that could reach a value of $760 million
for twelve initial launches of various Bigelow
Aerospace hardware.74 This contract offer is an
incentive for the development of new commercial
orbital transportation systems, and for Bigelow
Aerospace as it begins to develop plans for the
mass production of its expandable, orbital habitats.75
2008 U.S. Commercial Space Transportation Developments and Concepts In-Space Technology
Federal Aviation Administration Office of Commercial Space Transportation 37
Conception of Bigelow modules
38 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Enabling Technologies
Organizations from industry and the government
have been working to develop launch vehicle com-
ponents that are substantially simpler, more flexible
and reliable, and less costly than legacy technolo-
gies. These efforts research projects in the areas of
air launch technologies, composite cryogenic fuel
tanks, propulsion systems, thermal protection sys-
tems, and vehicle recovery systems. This chapter
reviews some of the accomplishments made in
2007 with emphasis given to those organizations
and technologies that have achieved significant test-
ing milestones.
Friction Stir Welding - Space Exploration Technologies
Corporation
Space Exploration Technologies Corporation
(SpaceX) uses friction stir welding during the con-
struction of the Falcon 9 launch vehicle. The Falcon
9’s first and second stage walls use a high-perform-
ance aluminum-lithium alloy. This is difficult and
disadvantageous to weld with traditional techniques
because the lightweight lithium vaporizes when
melted, changing the alloy composition and produc-
ing a joint that is far weaker than the adjoining
material. Friction stir welding forms a metal-to-
metal joint without melting, using only friction and
pressure. Thus, the alloy composition remains unaf-
fected and retains its strength. This allows for the
creation of some of the lightest and strongest possi-
ble metal alloy tanks.76
Composite Tanks - Microcosm, Inc.
In 2007, Microcosm, Inc., of Hawthorne,
California, continued development of a cryogenic
composite LOX tank under SBIR Phase 2 funding.
Microcosm successfully tested a 64-centimeter (25-
inch) diameter, all-composite LOX tank to nearly
four times its operating pressure of 3,790 kilopas-
cals (550 pounds per square inch). Testing occurred
at cryogenic temperatures using liquid nitrogen.
The new materials technology used for the tank
comes from Composite Technology Development
Inc. of Lafayette, Colorado. A month later,
Microcosm announced the successful completion of
final qualification tests on the full-scale, all-com-
posite cryogenic LOX tank for the Sprite SLV. This
time the testing was done for a full-scale, 107-cen-
timeter (42-inch diameter), all-composite, LOX
tank to nearly four times its operating pressure of
3,790-kilopascals (550-pounds per square inch).
Microcosm’s tank design and manufacturing
method prevents gas permeation/leakage, and man-
ages the typical micro-cracking that has always
been the problem with all-composite tanks at cryo-
genic temperatures. The tank design allows for
reduction in the weight of the propellant tanks for
Sprite and increases the mass to orbit by over 30
percent. Microcosm intends to offer this technology
in a range of sizes as well as custom-made pressure
vessels for industrial applications where ultra-high,
strength-to-weight ratio is important. The composite
tank is scheduled to be flight proven in early
2008.77
Solid Engines - Alliant Techsystems, Inc.
ATK was named the prime contractor by
NASA for the development of the Ares I first stage
in December 2005. The design of the Ares I first
Enabling Technologies
Falcon 9 first stage
Microcosm Composite Tanks
stage will primarily use existing Space Shuttle solid
rocket motor technology; however, ATK is develop-
ing new components to increase performance.
Improvements under development in 2007 include
an enhanced propellant grain shape in the forward
section of the motor and a larger diameter nozzle
throat. The core tooling used to achieve the new
propellant shape is in manufacturing.78 Two mock-
ups of a section located at the top of the motor
between the first and second stages, called the for-
ward skirt, have been constructed. The forward
skirt mockups will simulate the physical space
available for the avionics and will be used to deter-
mine the optimal required space and placement of
the electronics.
In August 2007, ATK was awarded a multi-
year $1.8 billion contract for the design, develop-
ment, test and evaluation of the Ares I first stage.
The multi-year contract extends through June 2013
and includes flight tests beginning in 2009. The
flight test in 2009 designated Ares I-X, will utilize
a modified four-segment Space Shuttle Solid
Rocket Booster with a fifth segment simulator. Five
ground tests of a new five-segment Ares I rocket
motor are scheduled in 2009-2011. Three Ares I
flight tests utilizing the new five-segment first
stages are scheduled in 2012 and 2013.79
Liquid Engines - AirLaunch LLC
AirLaunch LLC, of Kirkland, Washington, is
developing Vapor Pressurization (VaPak) LOX- and
propane-powered upper stage engines for its
QuickReach Small Launch Vehicle (SLV) as part of
the Falcon SLV program..
AirLaunch LLC conducted a 191-second
engine test in March 2007, the longest VaPak
engine burn in history. As of November 2007,
AirLaunch had conducted 55 test firings of its
propulsion system, all using VaPak. The
QuickReach second stage engine has been fired 50
times, totaling over 400 seconds, on the Horizontal
Test Stand (HTS), in addition to several cold flow
tests. Five test fires, totaling 315.5 seconds, have
been performed on the Vertical Test Stand (VTS)
with the QuickReach Integrated Second Stage
(IS2), in addition to several propellant loading and
conditioning tests.80 The IS2 firings incorporated
ground propellant loading operations and flight-
type avionics, software, and systems. Transition of
liquid oxygen to gaseous oxygen, a feature of
VaPak, has been observed in test fires on both the
HTS and VTS.
In July 2007, DARPA and the USAF jointly
agreed to fund Phase 2C at a value of $7.6 million.
Phase 2C milestones include upgrades to hardware,
instrumentation, and test stands; and a series of test
fires on the HTS to gather data on engine perform-
ance and on the VTS to more comprehensively
characterize second stage performance.81
Liquid Engines – Garvey SpacecraftCorporation
Garvey Spacecraft Corporation (GSC) is a
small aerospace R&D company, formed in 1993,
that is focusing on the development of advanced
space technologies and launch vehicle systems.
GSC conducts research and development in partner-
ship with a variety of organizations. The most
notable of these partnerships has been the
California Launch Vehicle Education Initiative
(CALVEIN) with California State University, Long
Beach (CSULB). Since getting started in early
Federal Aviation Administration Office of Commercial Space Transportation 39
Enabling Technologies 2008 U.S. Commercial Space Transportation Developments and Concepts
Five-Segment Motor Test
AirLaunch Hot Fire Test on VTS
2001, the CALVEIN work has resulted in numerous
static fire tests and 15 flight tests, including devel-
opment of the CSULB aerospike engine as well as
the more recent missions involving the prototype
RLV test bed.
In September 2007, under the sponsorship of
the U.S. Department of Labor and the California
Space Authority’s Workforce Innovation in
Regional Economic Development (WIRED) pro-
gram, the launch of Prospector 8A (P-8A) took
place in the Mojave Desert. The primary goal of the
flight was to test the new 20,000-newton (4,500-
pound-force) thrust engine that GSC/CSULB has
been developing for the past year. Programmatic
objectives of the test included the creation of men-
toring experiences in hardware development for
aerospace students from CSULB, Stanford, and
other WIRED partners, as well as the manifesting
of payloads from academic, government, and com-
mercial organizations. The flight of Prospector 8A
ended prematurely when excessive fluttering result-
ed in failure of the stabilization fins. Lessons
learned from the P-8 flight are now being applied
by GSC to the development of the Prospector 9
prototype RLV under a Phase 2 SBIR with the Air
Force. In 2007 GSC began practicing and evaluat-
ing water recovery techniques to expand the scope
of their RLV operations. Present plans call for
GSC to conduct a test flight in 2008.82
Liquid Engines – Northrop GrummanCorporation
Northrop Grumman successfully tested a new
type of rocket engine specifically designed to use
oxygen and methane propellants that range from
all-gas to all-liquid at the inlet to the thruster. The
new engine design was developed under contract to
NASA Glenn Research Center’s Cryogenic
Reaction Control Engine program. The engine,
dubbed the TR408, ensures that the fuel and oxidiz-
er fully vaporize by passing the propellants through
cooling passages located in the thrust chamber wall
before injecting them into the chamber for combus-
tion. This technique ensures consistent performance
and combustion stability. Previous rocket engine
designs using propellant to cool the chamber do not
vaporize any of the propellant or may only vaporize
one of the propellants, typically the fuel. The
TR408 uses a simple design consisting of only two
propellant valves, no moving parts other than the
valves, and contains a built-in spark igniter to initi-
ate combustion of the injected propellants.
Northrop Grumman announced in November
2007 that the TR408 had performed more than 50
separate tests demonstrating operating stability and
an ample design margin for the 440-newton (100-
pounds-force) engine. Upcoming test will attempt
to operate the engine at a steady-state specific
impulse of 340 seconds.83
Liquid Engines – Pratt & WhitneyRocketdyne, Inc.
NASA awarded Pratt & Whitney Rocketdyne,
Inc. (PWR) a $1.2 billion contract in July 2007 to
design, develop, and test a J-2X engine that will
power the upper stage of the Ares I and Ares V
launch vehicles. Powered by liquid oxygen and liq-
uid hydrogen, the J-2X is an evolved variation of
two historic predecessors: the J-2 upper stage
engine, that propelled the Apollo-era Saturn IB and
Saturn V rockets to the Moon in the 1960s and
1970s, and the J-2S, a simplified version of the J-2
developed and tested in the early 1970s but never
flown. The J-2S turbopumps and related machinery
were demonstrated in the 1990s on the X-33
aerospike engine. The J-2X main injector hardware,
a major component of the engine, is similar to the
J-2 engine injector. Engineers at NASA’s Marshall
Space Flight Center conducted hot-fire tests on sub-
scale injector hardware in 2006 as part of an effort
to investigate design options that would maximize
performance of the J-2X engine for the Ares upper
stages. The J-2X ignition system also will be a
modified version of the system on the J-2 engine.
Tests of an augmented spark igniter were conducted
in 2006 at Marshall.84 In December 2007, NASA
began testing core components of the J-2X on the
A-1 Test Stand at NASA’s John C. Stennis Space
40 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Enabling Technologies
P-8A Static Fire Test
Center near Bay St. Louis, Mississippi. The tests
focused on the engine’s powerpack a gas generator
and turbopumps that perform the rocket engine's
major pumping and combustion work. During the
test, engineers ran liquid oxygen and liquid hydro-
gen through the powerpack, monitoring its ducts,
valves, and lines to verify the tightness of seals in
the oxidizer lines and pumps. All test objectives
were met with no anomalies noted.85
The J-2X will provide an estimated 1,308,000
newtons (294,000 pounds-force) of thrust to power
the Ares vehicles. The contract includes ground and
test flight engines and extends through December
31, 2012.86 The first integrated J-2X engine systems
test is scheduled for 2010.
Liquid Engines – Space Exploration Technologies
Corporation
In 2006, SpaceX began working on the
Merlin 1C engine, a regeneratively-cooled succes-
sor to the ablatively-cooled Merlin 1A engine. The
regeneratively-cooled Merlin 1C uses rocket pro-
pellant grade kerosene (RP-1), a refined form of jet
fuel, to cool the combustion chamber and nozzle
before combining it with the liquid oxygen to create
thrust. This cooling allows for higher performance
without significantly increasing engine mass. The
Merlin 1C engine will be used in upcoming Falcon
1 launches.87 The Merlin 1C will also be used for
the first and second stage of the Falcon 9.
During 2007, 125 hot fire tests were conduct-
ed on the Merlin 1C engine for a combined run
time exceeding 3,000 seconds. In November 2007,
SpaceX announced that it had completed develop-
ment of the Merlin 1C.88 In its current Falcon 9
first-stage configuration, the Merlin 1C has a thrust
at sea level of 423,000 newtons (95,000 pounds-
force), a vacuum thrust of over 480,000 newtons
(108,000 pounds-force), vacuum specific impulse
of 304 seconds and sea level thrust-to-weight ratio
of 92. In generating this thrust, the Merlin 1C con-
sumes 159 kilograms per second (350 pounds per
second) of propellant. The chamber and nozzle are
cooled by 45 kilograms per second (100 pounds per
second) of kerosene. The kerosene is capable of
absorbing 10 megawatts of heat energy. A planned
turbopump upgrade in 2009 will improve the thrust
by over 20 percent and the thrust to weight ratio by
approximately 25 percent.89
The Merlin 1C engine will power SpaceX’s
next Falcon 1 mission, scheduled to lift off in early
2008. SpaceX’s far
larger Falcon 9 rock-
et, now in develop-
ment, will employ
nine Merlin engines
on its first stage. A
vacuum version of
the Merlin 1C, with
a larger bell nozzle
and some additional
features, will be
used on the Falcon
9’s upper stage.90 In
2008, SpaceX targets
to build approxi-
mately 50 booster
engines, a number
that exceeds the out-
put of every country
except Russia.91
Federal Aviation Administration Office of Commercial Space Transportation 41
Enabling Technologies 2008 U.S. Commercial Space Transportation Developments and Concepts
J-2 Awaits Testing on the A-1 Test Stand
Merlin 1C Test Firing
Liquid Engines – XCOR Aerospace Inc.
XCOR Aerospace, Inc. headquartered in
Mojave, California, specializes in developing
engines and propulsion systems for use on launch
vehicles and spacecraft. In May 2006, XCOR won
a contract from ATK to develop a 33,300-newton
(7,500-pound-force) methane-fueled engine as a
prototype for potential use on NASA’s Orion space-
craft. The ATK-XCOR methane engine, also known
as the 5M15, will build upon XCOR’s existing
engines. According to XCOR, the engine serves
several purposes, including validation of key engine
design elements, such as the regeneratively cooled
chamber/throat assembly, the stability and perform-
ance of the injector, and the reliability of ignition.
The 5M15 will incorporate a number of design fea-
tures for safety and reliability, critical for human-
rated applications, that were demonstrated on previ-
ous XCOR engine designs. Finally, the design is
modular, facilitating rapid test of new components
during development, and enabling modification for
future exploration applications. Testing of the 5M15
began in Mojave in January 2007.92 In November
2007, Time magazine recognized the potential of
the 5M15 by making the methane-powered rocket
an “Invention of The Year” award winner.93 In
December 2007, XCOR Aerospace and ATK
announced the completion of testing on the 5M15.94
In October 2007 at the X PRIZE Cup, video
was shown of the first test flights of the Rocket
Racing League’s X-Racer vehicle. The X-Racer is
propelled by an XCOR-developed 4K14 engine that
produces 6,700 newtons (1,500 pounds-force) of
thrust. The 4K14 uses a regeneratively-cooled LOX
and pump-fed kerosene system. The X-Racer air-
frame is based on a Velocity airplane kit.95
Liquid RCS Thruster – Orion Propulsion, Inc.
Orion Propulsion, Incorporated, of Huntsville,
Alabama, announced in December 2007, the suc-
cessful completion of the first series of hot-fire tests
of a 440-newton (100-pound-force) oxygen-
methane thruster module. Development of the
thruster is funded by a NASA SBIR Phase 2 grant
awarded in October 2006. The purpose of the
thruster module proj-
ect is to design, fab-
ricate, and demon-
strate the use of
composite cryogenic
tanks integrated into
a propulsion system
that is representative
of future mission
requirements, such
as NASA’s Orion
Crew Exploration
Vehicle, Lunar
Lander, and long
duration space mis-
sions. The system
uses NASA-provid-
ed composite tanks,
which have under-
gone extensive cryo-
genic testing with
multiple cryogenic
fluids, including liq-
uid oxygen, liquid
nitrogen, and liquid
helium.
This engine offers advantages over existing
RCS thrusters, including flexibility, reusability, and
high performance. The simple configuration and
conventional manufacturing techniques contribute
to cost, weight, and risk reductions.96 The next step
on the thruster module effort is to perform a series
of extended storage tests on the cryogenic tanks.
Orion and NASA will continue hot-fire testing of
the module with gaseous and cryogenic propellants.
The system will be operated under the conditions of
a pressurized propellant system and under the con-
ditions of saturated propellants operating in a blow-
down mode.97
42 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Enabling Technologies
XCOR XR-5M15 Test Fire
Orion Thruster Test
Federal Aviation Administration Office of Commercial Space Transportation 43
Liquid RCS Thruster – Space Exploration Technologies
Corporation
SpaceX is developing a spacecraft thruster
called Draco that generates 400 newtons (90
pounds-force) of thrust. The Draco thruster is
fueled by a common aerospace bipropellant combi-
nation, monomethyl hydrazine and nitrogen tetrox-
ide (MMH/NTO). The SpaceX Dragon crew and
cargo spacecraft will have a total of 18 Draco
thrusters for both attitude control and orbital
maneuvering functions. Draco thrusters will also be
used on the Falcon 9 second stage for maneuvering
and deorbiting. In 2007, SpaceX’s propulsion team
completed the first Draco development engine, and
in 2008 will begin testing at their new MMH/NTO
test facilities in central Texas.98
Launch Abort System – OrbitalSciences Corporation
Orbital Science Corporation announced in
September 2006 that it will build the Launch Abort
System (LAS) for the NASA Orion CEV. Orbital is
a member of the Lockheed Martin-led team select-
ed to construct the Orion CEV and will receive
approximately $250 million under subcontract to
Lockheed Martin to construct the LAS.99 The LAS
will be composed primarily of solid rocket motors,
separation mechanisms, canards, and an adapter
structure. The LAS will provide escape capability
for the Orion crew from pad operations through
ascent. The new design, using Orbital’s small
launch vehicle technology, will improve flight crew
safety as compared to current human space flight
systems.
On November 14, 2007, NASA broke ground
on a new test launch pad at the U.S. Army’s White
Sands Missile Range, N.M., that will be the site of
a series of tests of a launch abort system for the
Orion CEV. The first of five planned abort tests is
scheduled from the new pad in September 2008.
Two tests are planned to evaluate the performance
of the launch abort system at ground level and three
tests will evaluate its performance at different alti-
tudes.100 The contract calls for a five-year develop-
ment program. Initial crewed flights to orbit are
planned during the 2012 to 2014 time period, fol-
lowed by a series of operational missions to the
International Space Station and the Moon.101
Scramjet Propulsion – Pratt & WhitneyRocketdyne, Inc.
Pratt & Whitney Rocketdyne, Inc., along with
its X-51A team members, including the U.S. Air
Force, DARPA, NASA, and the Boeing Company,
demonstrated operation and performance of the X-1
scramjet engine in the first simulated flight at Mach
5 of the X-51A. The X-1 demonstrator engine, des-
ignated the SJX61-1, is a hydrocarbon-fueled
scramjet featuring X-51A flight hardware. The X-
51A flight test program plans to demonstrate scram-
Enabling Technologies 2008 U.S. Commercial Space Transportation Developments and Concepts
Draco Thruster
Conceptual Orion Launch Abort System X-1 Scramjet Test
jet engine technology within the Mach 4.5-6.5
range with four flight tests beginning in 2009.
According to PWR, the program will set the foun-
dation for several hypersonic applications including
access to space. Additional tests in early 2008 will
verify engine performance and operability across
the X-51A flight envelope.102
Propellant Production – Andrews Space, Inc.
Andrews Space, Inc., of Seattle, Washington,
has developed an in-flight propellant collection sys-
tem, the “Alchemist” Air Collection and
Enrichment System (ACES), which generates LOX
through the separation of atmospheric air. The
ACES takes high-pressure air from turbofan jet
engines flying at subsonic speeds and cools it by
passing the air through a series of heat exchangers
cooled by both oxygen-depleted air and liquid
hydrogen. Then, using a fractional distillation
process, liquid oxygen is separated and stored in
propellant tanks for use by liquid hydrogen and liq-
uid oxygen rocket engines.
In March 2006, DARPA/AFRL awarded
Andrews Space, Inc., additional funding to demon-
strate operational capabilities of its Alchemist
ACES. Under the new contract, valued close to
$350,000, Andrews will advance the state-of-the-art
and demonstrate critical ACES components and
operating parameters. This bridge funding is meant
to permit early demonstration of the technologies
required and to make significant program risk
reductions. Development and demonstration of
these technologies offers a hybrid approach to rock-
et propulsion, which can significantly reduce take-
off gross weight.103 In 2007, Andrews continued
testing of the ACES system and successfully vali-
dated that rotary packing material could be used in
the fractional distillation process at forces in excess
of 1-G.104
Air Launch Method – AirLaunch LLC
In July 2006, AirLaunch LLC dropped a full-
scale simulated QuickReach rocket, weighing
almost 33,000 kilograms (72,000 pounds) and
measuring 20 meters (66 feet) in length, from an
Air Force C-17 cargo plane as part of the
DARPA/Air Force Falcon SLV Program. The
unmodified C-17A aircraft released the test article
at an airspeed of 600 kilometers/hour (330 knots)
from an altitude of 9,700 meters (32,000 feet). The
drop was third in a series of envelope expansion
tests to verify the ability of the C-17 safely to deliv-
er AirLaunch’s full-scale, full-weight QuickReach
rocket to its operational launch altitude. Previous
tests took place in June 2006 and in September
2005. Each test set a new C-17 record for the
longest and heaviest single item dropped from the
aircraft.105 The initial test in 2005 demonstrated the
QuickReach release technology, including proof
that the nose of the rocket does not hit the roof of
the C-17A airplane as the booster leaves the carrier
aircraft. The Falcon SLV program’s Phase 2C
includes a launch demonstration that could occur in
2008. AirLaunch did not conduct any further tests
of the unique air launch system in 2007, instead
focusing on development of propulsion systems for
the QuickReach as detailed earlier in this chapter.106
Thermal Protection System – Andrews Space, Inc.
In December 2007, Andrews Space, Inc.,
announced the development and testing of new
material for enabling advanced thermal protection
systems. The tests, conducted at the NASA Ames
Research Center arc-jet facility as part of a NASA
44 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Enabling Technologies
Andrews ACES Test
QuickReach Drop Test
Phase 2 SBIR to develop lightweight ballute
designs, identified new materials that can be used
to enable thermal protection systems for non-rigid
aerosurfaces. A ballute is a pressure-stabilized,
inflatable membrane that provides a large, blunt,
high-drag surface for aerobraking systems. Ballutes
offer significant advantages over rigid shells for
aerocapture and reentry of spacecraft by providing
simplified packaging and lower total weight.
Traditional ballute designs use several layers of
Nextel fabric with insulating layers of Kapton and
Kevlar structural backing. Andrews is developing
lighter weight designs using thinner materials and
transpiration cooling. The goal of the transpiration-
cooled TPS design is to reduce the mass of the bal-
lute TPS system by 20 percent over traditional,
purely insulative solutions. Experimental data will
be used to refine the ballute design and develop a
concept to enable larger operational systems.107
Thermal Protection System – Boeing
Boeing completed a developmental, 5-meter
(16-feet) wide heat shield for NASA’s Orion CEV
in November 2007. The heat shield uses Phenolic
Impregnated Carbon Ablator (PICA) material man-
ufactured by Fiber Materials, Inc. of Biddeford,
Maine, under contract to Boeing. PICA is a modern
TPS material developed by NASA’s Ames Research
Center and has the advantages of low density cou-
pled with efficient ablative capability at high heat
flux. PICA is being considered for Orion’s heat
shield due to its proven performance on NASA’s
Stardust spacecraft heat shield. PICA’s thermal
characteristics will enable the CEV to survive the
high reentry velocity associated with Earth reentry
following a lunar mission.108
Stage Recovery System – Alliant Techsystems, Inc. & United
Space Alliance, LLC
ATK and United Space Alliance successfully
tested in 2007 the world’s largest rocket stage
recovery parachute system. In September and
November 2007, the 46-meter (150-foot) diameter,
900-kilogram (2,000-pound) parachute carried a
19,000-kilogram (42,000-pound) weighted test unit
safely to the Earth.109 The parachute is derived
from the 41-meter (136-foot) main parachute cur-
rently used on the Space Shuttle Solid Rocket
Boosters. The larger parachute will be used by the
new five-segment solid rocket booster being devel-
oped for the Ares I first stage. The first Ares test
flight, Ares I-X, a full-scale launch vehicle with
inert upper stage, will use the new parachute. Ares
I-X is scheduled to launch in April 2009.110
Federal Aviation Administration Office of Commercial Space Transportation 45
Enabling Technologies 2008 U.S. Commercial Space Transportation Developments and Concepts
Prototype Heat Shield
Parachute Testing at Yuma Proving Ground
Launch and reentry sites—often referred to as
“spaceports”—are the nation’s gateways to and
from space. Although individual capabilities vary,
these facilities may house launch pads and runways
as well as the infrastructure, equipment, and fuels
needed to process launch vehicles and their pay-
loads before launch. The first such facilities in the
United States emerged in the 1940s when the feder-
al government began to build and operate space
launch ranges and bases to meet a variety of nation-
al needs.
While U.S. military and civil government
agencies were the original and still are the primary
users and operators of these facilities, commercial
payload customers have become frequent users of
federal spaceports. Federal facilities are not the
only portals to and from space. Indeed, the com-
mercial dimension of U.S. space activity is evident
not only in the numbers of commercially procured
launches but also in the presence of non-federal
launch sites supplementing federally operated sites.
Since 1996, the FAA has licensed the operations of
six launch or reentry sites, some of which are co-
located with federal facilities. These spaceports
serve both commercial and government payload
owners.
Table 1 shows which states have non-federal,
federal, and proposed spaceports. Figure 1 shows a
map of U.S. spaceports and launch sites. Non-fed-
eral and federal U.S. spaceports capable of support-
ing launch and landing activities are described. A
subsection detailing state and private proposals for
future spaceports is also included.
Non-Federal Spaceports
While the majority of licensed launch activity
still occurs at U.S. federal ranges, significant future
launch and landing activity may originate from
spaceports operated by private entities or state and
local governments. For a U.S. person or institution
that is a non-federal entity to operate a launch or
reentry site in the U.S. or U.S. territories, it is nec-
essary to obtain a license from the federal govern-
ment through the FAA. To date, the FAA has
licensed six non-federal launch sites. Three are co-
located with federal launch sites, including the
California Spaceport at Vandenberg Air Force Base,
California; the Cape Canaveral Spaceport at Cape
Canaveral Air Force Station, Florida; and the Mid-
Atlantic Regional Spaceport at Wallops Flight
Facility, Virginia. In addition, Blue Origin utilizes
an exclusive use launch site in western Texas that is
not an FAA licensed spaceport. Similarly, Sea
Launch also does not need an FAA launch site
operator license. The first orbital launch from an
FAA-licensed site occurred on January 6, 1998,
when a Lockheed Martin Athena 2, carrying
NASA’s Lunar Prospector spacecraft, successfully
lifted off from Cape Canaveral Spaceport. Table 2
summarizes the characteristics of non-federal
spaceports.
Blue Origin West Texas Launch Site
Blue Origin West Texas launch site is a pri-
vate property owned by Jeff Bezos, the founder of
Amazon.com and Blue Origin, LLC. After purchas-
ing almost 66,800 hectares (165,000 acres) of
desert 40 kilometers (25 miles) north of Van Horn,
in Culberson County, Texas, the entrepreneur
expressed interest in building and operating a pri-
vate spaceport. Blue Origin proposes to launch
RLVs on suborbital, ballistic trajectories to altitudes
in excess of 99,000 meters (325,000 feet). To con-
duct these operations, Blue Origin would construct
a private launch site, including a vehicle processing
46 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Spaceports
Table 2: Spaceport Summary by State
State Non-federal Federal Proposed
Alabama
Alaska
California
Florida
Kwajalein
New Mexico
Oklahoma
Texas
Virginia
Washington
Wisconsin
Wyoming
* Blue Origin utilizes an exclusive use launch site located in Texas.
Federal Aviation Administration Office of Commercial Space Transportation 47
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Table 3: Non-federal Spaceports Infrastructure and Status
Spaceport Location Owner/Operator Launch Infrastructure Development Status
Blue Origin West
Texas Launch Site
Culberson
County, Texas
Blue Origin No known infrastructure at this time. Blue Origin plans to construct a private launch
site, including a vehicle processing facility,
launch complex; vehicle landing and recovery
areas; and space flight participant training
facility. Blue Origin received the first
experimental permit for a reusable suborbital
rocket in September 2006 and executed a test
launch in November 2006. Subsequent flights
followed in March and April 2007.
California
Spaceport
Vandenberg
AFB, California
Spaceport
Systems
International
Existing launch pads, runways, payload
processing facilities, telemetry, and
tracking equipment.
SLC 8 modified to support Minotaur IV.
Cape Canaveral
Spaceport
Cape
Canaveral,
Florida
Space Florida One orbital launch complex with a
remote control center, one suborbital
launch complex with two pads and a
blockhouse, an off-site solid rocket
motor storage that includes heavy rail
access, a 27-m (90-ft) high bay with
overhead cranes, a storage building,
and a 5,200-m2 (50,000-ft2) RLV
support hangar.
The quadra-axial static rocket test stand is
under construction. It can accommodate
engines up to 44,500 newtons (10,000 lbf)
thrust.
Kodiak Launch
Complex
Kodiak Island,
Alaska
Alaska Aerospace
Development
Corporation
Launch control center, payload
processing facility, and integration and
processing facility, orbital and suborbital
launch pads, and maintenance and
storage facilities.
In 2006, AADC added eight additional
redundant telemetry links to its range safety
and telemetry system. Future expansion plans
include building a second suborbital launch
pad and a motor storage facility, and
increasing fiber-optic bandwidth to the
continental United States.
Mid-Atlantic
Regional Spaceport
Wallops Island,
Virginia
Virginia
Commercial Space
Flight Authority
Two orbital launch pads, payload
processing and integration facility
vehicle storage and assembly buildings,
mobile liquid fueling capability, on-site
and downrange telemetry and tracking,
and payload recovery capability.
Site is operational. Currently it is conducting
the planning and investigation of the
expansion of capability to include heavier lift in
support of commercial cargo to LEO
operations.
Mojave Air and
Space Port
Mojave,
California
East Kern Airport
District
Air traffic control tower, three runways,
rotor test stand, engineering facilities,
high bay building. Easy access to
restricted airspace. Space zoned
specifically for rocket motor
development and testing.
Infrastructure upgrades for 2007 were affected
by the July 26 explosion. Funding has been
received for the construction of a more
reliable water delivery system that includes
extension and upgrade of the water
distribution system, as well as construction of
an additional water storage tank. The
construction is expected to be completed by
spring 2008.
Oklahoma
Spaceport
Washita
County,
Oklahoma
Oklahoma Space
Industry
Development
Authority
A 4,115-m (13,500-ft) runway; 5,200-m2
(50,000-ft2) manufacturing facility;
2,7850-m2 (30,000-ft2) maintenance and
painting hangar; 6 commercial aircraft
hangars, including a 2,787-m2 (30,000-
ft2) maintenance and paint facility; 39-
ha (96-a) of concrete ramp, control
tower, crash and rescue facility; and
435-km2 (168-m2) of land available for
further construction.
The Clinton-Sherman AFB at Burns Flat was
designated as the future spaceport. OSIDA
received a Launch Site Operators License
from the FAA in June 2006. In June 2007,
Armadillo launched the first flight under the
new experimental permit rules from Oklahoma
Spaceport.
facility, launch complex, vehicle landing and recov-
ery area, spaceflight participant training facility,
and other support facilities.111
After reviewing the environmental assessment
and finding of no significant impact for the pro-
posed Blue Origin West Texas launch site, FAA
issued to Blue Origin the first experimental permit
for a reusable suborbital rocket in September 2006.
This type of permit was first authorized by the
Commercial Space Launch Amendments Act of
2004. The vehicle to be tested will be unmanned
and will be launched and landed vertically during
tests. The permit granted to Blue Origin is a one-
year, renewable permit, allowing for unlimited
launches. Such permits are intended to allow launch
vehicle developers to flight test their designs.112 The
first flight of Goddard, a subscale protype of the
company’s planned New Shepard vehicle, took
place in November 2006; subsequent flights of
Goddard took place in March and April 2007.
California Spaceport
On September 19, 1996, the California
Spaceport became the first commercial spaceport
licensed by the FAA. The California Spaceport
offers commercial launch and payload processing
services and is operated and managed by Spaceport
Systems International (SSI), a limited partnership
of ITT Federal Service Corporation. Co-located at
VAFB on the central California coast, SSI signed a
25-year lease in 1995 for 0.44 square kilometers
(0.17 square miles) of land. Located at 34º North
latitude, the California Spaceport can support a
variety of mission profiles to low-polar-orbit incli-
nations, with possible launch azimuths ranging
from 220° to 165°.
Construction of the California Spaceport com-
mercial launch facility began in 1995 and was com-
pleted in 1999. The design concept is based on a
“building block” approach. Power and communica-
tions cabling were routed underground to provide a
launch pad with the flexibility to accommodate a
variety of launch systems. The current Space
Launch Complex 8 (SLC-8) configuration consists
of the following infrastructure: pad deck, support
equipment building, launch equipment vault, launch
duct, launch stand, access tower, communications
equipment, and Integrated Processing Facility (IPF)
launch control room, as well as the required
Western Range interfaces needed to support a
launch. During 2007, the spaceport has been
upgrading both the IPF and SLC-8 to meet user
requirements, and thus has not been able to support
48 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
California Spaceport
Vandenberg AFB
-Kennedy Space Center
-Cape Canaveral Air Force
Station
-Cape Canaveral Spaceport
Mid-Atlantic
Regional Spaceport
Wallops Flight
Facility
Edwards AFB
Mojave Air and Space Port
White Sands Missile Range
Spaceport America
West Texas Spaceport
♦♦
•• Kodiak Launch Complex
♦♦
♦♦
♦♦
∗∗♦♦
••
••
••
Oklahoma Spaceport
∗∗
∗∗
∗∗
∗∗
••
♦♦
Key:
U.S. Federal Spaceport
Non-Federal Spaceport
Proposed Non-Federal Spaceport
South Texas Spaceport
••
Sea Launch Platform
Equatorial Pacific Ocean
••
♦♦ Reagan Test Site
Kwajalein Atoll, Marshall Islands
∗∗ Spaceport
Washington
∗∗
Spaceport Sheboygan
∗∗Spaceport Alabama
••
Chugwater Spaceport
∗∗
Cecil Field SpaceportBlue Origin
Exclusive Use Launch Site
••
California Spaceport
Vandenberg AFB
-Kennedy Space Center
-Cape Canaveral Air Force
Station
-Cape Canaveral Spaceport
Mid-Atlantic
Regional Spaceport
Wallops Flight
Facility
Edwards AFB
Mojave Air and Space Port
White Sands Missile Range
Spaceport America
West Texas Spaceport
♦♦
•• Kodiak Launch Complex•• Kodiak Launch Complex
♦♦
♦♦
♦♦
∗∗♦♦
••
••
••
Oklahoma Spaceport
∗∗
∗∗
∗∗
∗∗
••
♦♦
Key:
U.S. Federal Spaceport
Non-Federal Spaceport
Proposed Non-Federal Spaceport∗∗
••
♦♦
∗∗
••
♦♦
Key:
U.S. Federal Spaceport
Non-Federal Spaceport
Proposed Non-Federal Spaceport
South Texas Spaceport
••
Sea Launch Platform
Equatorial Pacific Ocean
••
♦♦ Reagan Test Site
Kwajalein Atoll, Marshall Islands
∗∗ Spaceport
Washington
∗∗
Spaceport Sheboygan
∗∗Spaceport Alabama
••
Chugwater Spaceport
∗∗
Cecil Field SpaceportBlue Origin
Exclusive Use Launch Site
••
Figure 1: U.S. Spaceports and Launch Sites
any launches from the SLC-8. The modifications
for SLC-8 to support the Minotaur 4 launch system
included upgrades to SLC-8 Mobile Access Tower
and the Launch Equipment Vault (LEV).113 The
modifications were completed on schedule, in
December 2007. The upgrades have been financed
through USAF government contracts as well as pri-
vate capitalization projects.114 When fully devel-
oped, SLC-8 will accommodate a wide variety of
launch vehicles, including the Minuteman-based
Minotaur and Castor 120-based vehicles such as the
Taurus.
California Spaceport supports satellite pro-
cessing for launches at SLC-2, SLC-3, SLC-6, and
SLC-8. Originally, the focus of the California
Spaceport’s payload processing services was on the
refurbishment of the Shuttle Payload Preparation
Room. Located near SLC-6, this large clean room
facility was designed to process three Space Shuttle
payloads simultaneously. Now, the facility is leased
and operated by the California Spaceport as the
IPF; payload-processing activities occur on a regu-
lar basis. The IPF has supported booster processing;
upper stage processing; encapsulation; and com-
mercial, civil, and military satellite processing and
their associated administrative activities. The IPF
can handle all customer payload processing needs.
This capability includes Delta II, Delta IV, and
Atlas V payloads as well as smaller USAF and
commercial payloads. During 2007, the spaceport
supported processing of classified payloads in the
IPF.
In 2001, SSI won a 10-year USAF satellite-
processing contract for Delta IV class 4- and 5-
meter (13- and 16-foot) payloads. This contract
complements an existing 10-year NASA payload-
processing contract for Delta II class 3-meter (10-
foot) payloads. SSI is working with several launch
providers for national missile defense support. The
National Reconnaissance Office has contracted with
SSI to provide payload processing until 2015. This
contract covers Delta IV and Atlas V EELV-class
payload processing support for multiple missions to
be launched from VAFB. NASA and commercial
Delta-class payloads are also processed at the IPF
for launch on the Delta II from SLC-2W at VAFB.
Cape Canaveral Spaceport
Space Florida was created on May 30, 2006,
when then-Florida Governor Jeb Bush approved
Florida House Bill 1489. Space Florida consoli-
dates the state’s previous space and aerospace enti-
ties and coordinates all space-related issues in
Florida. Under an arrangement between the federal
government and Space Florida, excess CCAFS
facilities were licensed to Space Florida for use by
commercial launch service providers on a dual-use,
non-interference basis.
Major infrastructure operated by Space
Florida at CCAFS includes Launch Complex-46
(LC-46), a refurbished Trident missile launch site.
LC-46 has been modified to accommodate a variety
Federal Aviation Administration Office of Commercial Space Transportation 49
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
California Spaceport SLC-8
Space Florida SLC-46 MAS
50 Federal Aviation Administration Office of Commercial Space Transportation
of small launch vehicles, and has already success-
fully launched the Athena 1 and Athena 2 rockets.
With further modifications, LC-46 could accommo-
date vehicles carrying payloads in excess of 1,800
kilograms (4,000 pounds) to LEO. During 2007,
Space Florida refurbished the LC-46 Mobile Access
Structure. This was a $100,000 investment,
financed through government appropriations.
As part of an overall effort to expand use of
the Cape for research, development, and education-
al activities, Space Florida obtained a five-year
license from the Air Force to use LC-47. This
launch complex was upgraded to support a signifi-
cant number of suborbital launch vehicles carrying
academic payloads for research and training pur-
poses. In May 2007, the construction of a quadra-
axial static rocket motor test stand started. The
stand will be capable of accommodating motors up
to 30 centimeters (12 inches) in diameter, with a
maximum average thrust of 53,400 newtons
(12,000 pounds-force). The delivery of this system
is expected in the spring of 2008.115
Space Florida’s Strategic Business Plan rec-
ommends upgrading and marketing the commercial
launch facilities at LC-46 at the Cape Canaveral
Spaceport, developing a spaceport operating model
to manage the Cape Canaveral Spaceport and other
Florida spaceports, and providing economic incen-
tive options to assist NASA COTS competitors.116
During 2007, Space Florida has contracted with
Reynolds, Smith, and Hills, an architecture, engi-
neering and planning firm, to develop an update of
its five-year Master Plan. The plan will be submit-
ted to the Florida Department of Transportation
(FDOT) and appropriate metropolitan planning
organizations for review of inter-modal impacts and
inclusion of eligible projects in FDOT’s five-year
work program. The update is expected to be com-
pleted by March 2008.117
The State of Florida has also developed the
Customer Assistance Service Program for the
Eastern Range (CASPER). This program is meant
to provide no-cost professional consultant guidance
to commercial launch service providers wishing to
operate from the USAF Eastern Range and NASA
Kennedy Space Center. CASPER provides guid-
ance on how to complete requirements documenta-
tion and how to navigate the flight safety approval
process in order to receive authorization to fly from
the Eastern Range.118
Although no launches took place from Cape
Canaveral Spaceport in 2007, Space Florida provid-
ed incentives to SpaceX as part of their NASA
COTS efforts. The State of Florida was instrumen-
tal in SpaceX securing a five-year license from the
USAF for LC-40 at CCAFS. Space Florida has pro-
vided over $600,000 worth of assistance to SpaceX
through economic incentives such as office space,
concept of operations design studies, and environ-
mental studies. Using CASPER, Space Florida has
also provided professional consultant services to
SpaceX to guide it in the development of range
documentation and flight safety systems to help it
secure required launch approvals and authoriza-
tion.119
In the future, Space Florida plans to incorpo-
rate a high-expansion foam fire-fighting system into
the RLV support hangar. The Cape Canaveral
Spaceport expects to receive between $7-10 million
in direct appropriations to support its operations
during fiscal year 2008.120
Kodiak Launch Complex
In 1991, the Alaska state legislature created
the Alaska Aerospace Development Corporation
(AADC) as a public company to develop aero-
space-related economic, technical, and educational
opportunities for the state of Alaska. In 2000, the
AADC completed the $40-million, two-year con-
struction of the Kodiak Launch Complex (KLC) at
Narrow Cape on Kodiak Island, Alaska. The first
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
FTG-03 Launch from Kodiak Launch Complex
licensed launch site not co-located with a federal
facility, KLC was also the first new U.S. launch site
built since the 1960s. Owned by the state of Alaska
and operated by the AADC, the KLC received ini-
tial funding from the USAF, U.S. Army, NASA,
state of Alaska, and private firms. Today, it is self-
sustaining through launch revenues and receives no
state funding; the state of Alaska provides tax-free
status and has contributed the land on which the
spaceport resides.
Kodiak has conducted eleven successful
launches since 1998. Located at 57º North latitude,
Kodiak Launch Complex occupies a 12.4-square-
kilometer (4.8-square mile) site 438 kilometers
(272 miles) south of Anchorage and 40 kilometers
(25 miles) southwest of the city of Kodiak. The
launch site itself encompasses a nearly five-kilome-
ter (three-mile) area around Launch Pad 1. Kodiak
provides a wide launch azimuth and unobstructed
downrange flight path. Kodiak’s markets are mili-
tary launches, government and commercial
telecommunications, remote sensing, and space sci-
ence payloads weighing up to 1,000 kilograms
(2,200 pounds). These payloads can be delivered
into LEO, polar, and Molniya elliptical orbits.
Kodiak is designed to launch up to Castor 120-
based vehicles, including the Athena 1 and 2, and
has been used on a number of occasions to launch
military suborbital rockets.
The Missile Defense Agency (MDA) conduct-
ed target missile launches from KLC in February
2006, September 2006, May 2007, and September
2007. A five-year contract was signed in 2003
between the Missile Defense Agency (MDA) and
AADC to provide launch support services for mul-
tiple launches in connection with tests of the
nation’s missile defense system.
Kodiak facilities include the Launch Control
Center; Payload Processing Facility, which includes
a Class-100,000 clean room, an airlock, and a pro-
cessing bay; Launch Service Structure and orbital
Launch Pad 1; Spacecraft and Assemblies Transfer
Facility and suborbital Launch Pad 2; Integration
and Processing Facility; and Maintenance and
Storage Facility. These facilities allow the transfer
of vehicles and payloads from processing to launch
without exposure to the outside environment. This
capability protects both the vehicles and the people
working on them from exterior conditions and
allows all-weather launch operations. Future expan-
sion plans include building a second suborbital
launch pad and a motor storage facility, and
increasing fiber-optic bandwidth to the continental
United States.
The KLC Range Safety and Telemetry System
(RSTS) was delivered in September 2003 and
upgraded in 2005. This RSTS consists of two fully
redundant systems: one for on-site, the other for
off-axis. Each part of the RSTS consists of two 5.4-
meter (17.7-foot) dishes with eight telemetry links
featuring command destruct capabilities. The
Kodiak RSTS number 1 system will be located on a
newly constructed multi-elevation antenna field that
also supports customer-unique instrumentation.
Mid-Atlantic Regional Spaceport
The Mid-Atlantic Regional Spaceport
(MARS) is designed to provide “one-stop-shop-
ping” for space launch facilities and services for
commercial, government, scientific, and academic
users. From its location on the Atlantic coast, this
spaceport can accommodate a wide range of orbital
Federal Aviation Administration Office of Commercial Space Transportation 51
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
NFIRE satellite mission launched from MARS
inclinations and launch azimuths. Optimal orbital
inclinations accessible from the site are between
38° and 60°; other inclinations, including Sun-syn-
chronous orbit (SSO), can be reached through in-
flight maneuvers.
The FAA issued a launch site operator’s
license to the Virginia Commercial Space Flight
Authority (VCSFA) in December 1997. In July
2003, Virginia and Maryland created a bi-state
agreement to operate, conduct future development
of, and promote the spaceport. The agreement also
renamed the spaceport, previously called the
Virginia Space Flight Center, to MARS.
MARS received $100,000 in July 2007 as fis-
cal year 2008 appropriation from Virginia. In addi-
tion, MARS benefits from the following incentives:
state sales and use tax exemptions on all goods
used, consumed or launched from MARS; state and
local personal property tax exemption on machinery
and equipment used as part of value added process
for vehicles and payloads launched from MARS;
state sponsored workforce training grants for new
employees of aerospace companies working at or
with MARS; state- and local-sponsored access to
flex space in the industrial park adjacent to MARS;
tort liability exclusion in Virginia courts resulting
from personal space flight activities at MARS; state
enterprise zone established at MARS to enable
rapid access to infrastructure development grants.
Also, VCSFA/MARS has bonding authority to issue
state tax exempt development bonds.
CSC-DynSpace LLC currently operates
MARS. In 1997, VCSFA signed a Reimbursable
Space Act Agreement with NASA to use the WFF
infrastructure to support commercial launches. This
30-year agreement allows MARS access to NASA’s
payload integration, launch operations, and moni-
toring facilities on a non-interference, cost reim-
bursement basis. NASA and MARS personnel work
together with commercial customers to facilitate
use of MARS facilities and services.
MARS has an official development plan,
approved by the VCSFA Board of Directors. The
plan was expanded in February 2007 to include the
capability to process and launch heavier payloads
and vehicles, such as those being developed in sup-
port of the NASA COTS initiative.121 The spaceport
is actively pursuing partnerships with space tourism
companies and has an interest in supporting future
RLVs, possibly using its launch pads or three run-
ways at WFF.122
MARS has two launch pads. Launch pad 0-B,
its first launch pad, was designed as a “universal
launch pad,” capable of supporting a variety of
small and medium ELVs with gross liftoff weights
of up to 283,000 kilograms (624,000 pounds) that
can place up to 4,500 kilograms (9,900 pounds)
into LEO. The Mobile Service Structure offers
complete vehicle enclosure, flexible access, and can
be readily modified to support specific vehicle
operations. The site also includes a complete com-
mand, control, and communications interface with
the launch range. In March 2000, MARS acquired a
second pad at WFF, launch pad 0A. MARS started
refurbishing launch pad 0A and its 25-meter (82-
foot) service tower in June 2000. Launch pad 0A
will support launches of small ELVs with gross
liftoff weights of up to 90,000 kilograms (198,000
pounds) and that can place up to 1,350 kilograms
(3,000 pounds) into LEO.
MARS is cooperating with NASA WFF in the
construction a $4-million logistics and processing
facility in the Wallops Research Park that includes
high bay and clean room environments. In conjunc-
tion with WFF, MARS constructed a mobile Liquid
Fueling Facility capable of supporting a wide range
of liquid-fueled and hybrid rockets. In 2007, MARS
completed the upgrade of the class-100,000 high
bay 1 of the new multi-purpose processing facility,
as well as added environmental control systems to
the launch pad 0-B Movable Service Structure.
While the improvements to the high bay were in
majority financed by the Federal government, the
launch pad construction was financed from the
spaceport revenue and cost approximately
$100,000.123 Future infrastructure improvement
plans include enhanced capability for pad 0-B
Movable Service Structure to accommodate addi-
tional launch vehicles.
Highlights for 2007 include the two orbital
launches from launch pad 0-B within a four-month
period. The first launch, of the USAF Space
Development and Test Wing (SDTW)
SDTW/AFRL TacSat 2 satellite, took place in
December 2006, while the second one, of a USAF
SDTW/MDA NFIRE satellite, happened in April
2007. The first launch was performed with only a
52 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Federal Aviation Administration Office of Commercial Space Transportation 53
five month call-up period for a launch vehicle never
before launched from MARS (Minotaur I). MARS
also contracted with NASA and the U.S. Air Force
for the NASA ALV-X1 launch in February 2008
and for USAF SDTW/AFRL TacSat 3 launch in
June 2008.124 Another highlight for 2007 is the pass-
ing of the Spaceflight Liability and Immunity Act,
Code of Virginia, Chapter 3, Title 8.01-227.8 et.al.in April of 2007.
Mojave Air and Space Port
Mojave Air and Space Port (formerly Mojave
Airport) in Mojave, California, became the first
inland launch site licensed by the FAA on June 17,
2004, allowing Mojave Air and Space Port to sup-
port suborbital launches of RLVs. The Kern
County, California, government established the
Mojave Airport in 1935. The original facility was
equipped with taxiways and basic support infra-
structure for general aviation. A short time after its
inception, the Mojave Airport became a Marine
Auxiliary Air Station. The largest general aviation
airport in Kern County, Mojave Air and Space Port
is owned and operated by the East Kern Airport
District (EKAD), which is a special district with an
elected Board of Directors and a General Manager.
Infrastructure at the Mojave Air and Space
Port includes an air traffic control tower with class
D airspace and three runways with associated taxi-
ways. Runway 12-30 is the primary runway for
large air carrier jet, high-performance civilian and
military jet aircraft, and horizontal launch space-
craft. An extension of runway 12-30 from 2,896
meters (9,502 feet) long to 3,810 meters (12,500
feet) was declared ready for use on December 5,
2006. Runway 8-26 is 2,149 meters (7,050 feet)
long and is primarily used by general aviation jet
and propeller aircraft. Runway 4-22 is 1,202 meters
(3,943 feet) long and is used by smaller general
aviation propeller aircraft and helicopters. The
extension of runway 12-30 and over $250,000
worth of repairs to the airfield and taxiways were
completed in November 2006. The cost of infra-
structure upgrades totaled $10.5 million with 95
percent of the funding provided by the FAA and 5
percent by EKAD.125
Mojave Air and Space Port serves as a
Civilian Flight Test Center with access to R-2508
restricted airspace. The airport has 162 hectares
(400 acres) of land available for immediate con-
struction. In addition, over 121 hectares (300 acres)
are zoned specifically for rocket motor testing and
development. Currently six companies are actively
developing and testing rocket motors.
Infrastructure upgrades planned for 2007 were
affected by the July 26 explosion during a cold-
flow test of a nitrous oxide propellant system for
SpaceShipTwo. The spaceport however received
funding from the Economic Development
Administration (EDA) to provide a more reliable
water delivery system for fire protection beyond a
single event occurrence. Such system includes
extension and upgrade of the water distribution sys-
tem as well as construction of an additional water
storage tank. The construction is expected to be
completed by spring 2008.
At the same time, Mojave is in the process of
upgrading its Automated Weather Observing
System (AWOS). The spaceport is also considering
plans for a crash fire rescue response facility that
would provide immediate support for RLVs that
land with technical difficulties or crew medical
emergencies.
Major facilities at the Mojave Air and Space
Port include the terminal and industrial area,
hangars, offices, maintenance shop, fuel services
facilities, aircraft storage, and reconditioning facili-
ties. Numerous large air carrier jet aircraft are
stored and maintained at the Mojave Air and Space
Port. The airport is home to a variety of organiza-
tions, including AVTEL, BAE Systems, Fiberset,
General Electric, Interorbital Systems, Masten
Space Systems, the National Test Pilot School,
Scaled Composites, Orbital Sciences, and XCOR
Aerospace.
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Mojave Air and Space Port
54 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Mojave Air and Space Port has been part of
two record-breaking events in this decade.
SpaceShipOne rocketed past the boundary of space
on September 29, 2004, and again on October 4,
2004, to win the $10 million Ansari X Prize. In
December 2005, the EZ-Rocket made a record-set-
ting point-to-point flight, departing from the
Mojave Air and Space Port and gliding to a touch-
down at an airport in neighboring California City.126
Oklahoma Spaceport
After seven years of development, in June
2006 the Oklahoma Spaceport became the sixth
commercial spaceport licensed by the FAA. In
1999, the Oklahoma state legislature created the
Oklahoma Space Industry Development Authority
(OSIDA). Directed by seven governor-appointed
board members, OSIDA promotes the development
of spaceport facilities and space exploration, educa-
tion, and related industries in Oklahoma. Currently,
the state of Oklahoma provides 100 percent of the
operational funding for OSIDA, but the organiza-
tion expects to be financially independent in the
future, particularly now that it holds a commercial
launch site operator license. Still, direct financial
support varies with specific needs for facility
upgrades or operations. OSIDA intends to submit a
request for one-time capital expenditures for facility
upgrades and expects to receive the support during
fiscal year 2008. Infrastructure development plans
for fiscal year 2008 include additional fencing for
the spaceport and development of a Fight
Operations Control Center, located in the OSIDA
headquarters. Besides state funding, NASA issued a
$915,000 grant to OSIDA for aerospace education
programs.
The FAA license allows OSIDA to provide
launch and support services for horizontally-
launched suborbital RLVs at the Clinton-Sherman
Industrial Airpark (CSIA) launch site, located near
Burns Flat. On December 5, 2006, the city of
Clinton conveyed ownership of the CSIA to
OSIDA. Existing infrastructure includes a 4,100-
meter (13,500-foot) runway, large maintenance and
repair hangars, utilities, a rail spur, and 12.4 square
kilometers (4.8 square miles) of open land. Existing
buildings could serve to house spaceplanes, manu-
facturing facilities, and even a passenger terminal.127
On July 13, 2007, the Oklahoma State Legislature
approved $2 million in funding for upgraded securi-
ty fencing and control tower improvements. Future
development plans include enhancing the facility’s
operational control room and hosting phased-array
radar tests.
Oklahoma’s site license clears the spaceport
for suborbital flights in a 110- x 270-kilometer (70-
x 170-mile) corridor of the prairie, with clearance
for launch vehicles to rise to the edge of outer
space.128 In June 2006, OSIDA signed a letter of
agreement with Fort Worth Air Route Traffic
Control Center that provides procedures for the
integration of licensed launch operations into the
National Airspace System from the Oklahoma
Spaceport.129 Thus, this launch site became the first
U.S. inland spaceport with an established fight cor-
ridor for space operations in the national airspace
system clear of military operating areas or restricted
airspace. This arrangement means that space vehi-
cles will not need military permission to operate
because the spaceport will have its own air space.
The spaceport license was granted for five years.
The Oklahoma Department of Commerce
offers several incentives to attract space-related
businesses. For example, a jobs program provides
qualifying companies with quarterly cash payments
worth up to five percent of its new taxable payroll
for up to ten years. Organizations also may qualify
for other state tax credits, tax refunds, tax exemp-
tions, and training incentives. Rocketplane Inc. and
TGV Rockets, Inc. have located in Oklahoma for
their launch vehicle developments. As the first cor-
poration that meets specific qualifying criteria,
including equity capitalization of $10 million and
creation of at least 100 Oklahoma jobs, Rocketplane
qualified for an $18-million, state-provided tax
credit. Another company pursuing space-related
activities in Oklahoma, Armadillo Aerospace, con-
ducted tethered operational testing at the Oklahoma
Spaceport with the vehicle that was used for the
Oklahoma Spaceport
2006 Northrop Grumman Lunar Lander competi-
tion.130 On June 2, 2007, Armadillo launched the
first flight under the new experimental permit rules
from a licensed spaceport. This flight performed a
complete Lunar Lander Challenge Level 1 (LLC1)
operational profile.
Federal Spaceports
Since the first licensed commercial orbital
launch in 1989, the federal ranges have continually
supported commercial launch activity in addition to
handling government launch operations. The impor-
tance of commercial launches is evident in the
changes taking place at federal launch sites. Launch
pads have been developed with commercial, feder-
al, and state government support at the two major
federal sites for U.S. orbital launches for the latest
generation of the Delta and Atlas launch vehicles.
Cape Canaveral Air Force Station and VAFB host
pads for the Delta II, Delta IV, and Atlas V.
Recognizing that the ranges are aging, the
U.S. government is engaged in range moderniza-
tion. This effort includes the ongoing Range
Standardization and Automation program, a key
effort to modernize and upgrade the Eastern Launch
and Test Range at CCAFS and the Western Range
at VAFB. The U.S. Air Force, Department of
Commerce, and FAA signed a Memorandum of
Agreement in January 2002 that established a
process for collecting commercial sector range sup-
port and modernization requirements, communicat-
ing them to the U.S. Air Force, and considering
them in the existing U.S. Air Force requirements
process. Table 3 summarizes the characteristics of
federal spaceports.
Cape Canaveral Air Force Station
The 45th Space Wing, headquartered at
Patrick AFB, conducts launch operations and pro-
vides range support for military, civil, and commer-
cial launches at CCAFS. The 45th Space Wing is
the host organization for Patrick AFB, CCAFS,
Antigua Air Station, Ascension Auxiliary Air Field,
and many mission partners. The Wing is part of Air
Force Space Command at Peterson AFB, Colorado,
and reports to the 14th Air Force at VAFB.
The 45th Space Wing manages the Eastern
Launch and Test Range (ELTR). The ELTR is used
to gather and process data on a variety of East
Coast launches and
deliver it to range
users. To accomplish
this task, the range
consists of a series
of tracking stations
located at CCAFS,
Antigua Air Station,
and Ascension
Auxiliary Air Field.
The range also uses
the Jonathan
Dickinson and the
Malabar Tracking
Annexes on the
Florida mainland.
These stations may
be augmented with a
fleet of advanced range instrumentation aircraft as
well as a site located in Argentia, Newfoundland.131
Users of CCAFS include the USAF, Navy,
NASA, and various private industry contractors.
The ELTR also supports Shuttle launches from
NASA KSC. With its mission partners, CCAFS
processes a variety of satellites and launches them
on Atlas V, Delta II, and Delta IV ELVs. The space-
port also provides support for the Space Shuttle
program and U.S. Navy submarine ballistic missile
testing.
During 2007, CCAFS supported Atlas V
launches of Orbital Express, NRO L-30, WGS 1,
and NRO L-24; the Delta II launches of THEMIS
1, Phoenix, Dawn, and NAVSTAR GPS 2RM-4 and
2RM-5; and one Delta IV Heavy launch of DSP 23.
Edwards Air Force Base
The original landing site for the Space
Shuttle, Edwards Air Force Base (EAFB),
California, is the home of more than 250 first
flights and about 290 world records. The first two
Shuttle flights landed on Rogers Dry Lake, a natu-
ral, hard-pack lakebed, measuring about 114 square
kilometers (44 square miles). Today, NASA uses
KSC as the primary landing site for the Space
Shuttle and uses EAFB as a backup site. EAFB is
the DoD’s premier flight test center, leading in
unmanned aerial vehicle (UAV), electronic warfare,
directed energy test capabilities, and testing of
future hypersonic vehicles.
Federal Aviation Administration Office of Commercial Space Transportation 55
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Cape Canaveral Air Force Station
Within the last 10 years, EAFB has been the
home of more than 10 experimental projects,
among them the X-33 airplane. The X-33 launch
site consisted of an X-33-specifc launch pad; a con-
trol center to be used for launch monitoring and
mission control; a movable hangar where the vehi-
cle was housed and serviced in a horizontal posi-
tion; and hydrogen, nitrogen, and oxygen storage
tanks. In 2006, three glide tests were successfully
completed on the DARPA-sponsored X-37
autonomous research vehicle.
56 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Spaceport Location Owner/Operator Launch Infrastructure Development Status
Cape Canaveral
Air Force Station
(CCAFS)
Cape
Canaveral,
Florida
U.S. Air Force Telemetry and tracking facilities, jet
and Shuttle capable runways,
launch pads, hangar, vertical
processing facilities, and assembly
building.
Site is operational.
Edwards AFB California, near
Mojave
U.S. Air Force Telemetry and tracking facilities, jet
and Shuttle capable runways,
reentry corridors, operations control
center, movable hangar, fuel tanks,
and water tower.
Site is operational.
Kennedy Space
Center
Cape
Canaveral,
Florida
NASA Launch pads, supporting Space
Shuttle operations, the Vehicle
Assembly Building (VAB), and the
Shuttle Landing Facility.
Environmental assessment underway for the
utilization of the Shuttle Landing Facility for
commercial suborbital and orbital spaceflight,
special purpose aviation, and other compatible
uses. During 2007, NASA signed a Space Act
Agreement with Starfighters Inc. for simulated
suborbital flight missions. Such missions would
generate data relevant for the analysis of the
environmental impact of suborbital and orbital
commercial spaceflight from the SLF.
Reagan Test Site Kwajalein
Island,
Republic of the
Marshall
Islands
U.S. Army Telemetry, radars, and optical
tracking systems, ship based
telemetry/safety system, mission
control facility, wideband CONUS
connectivity, multiple safety
systems and launch facilities,
runway, warehouse and industrial
use space, user and engineering
office space.
Site is operational. New launch pad on Omelek
Island completed in 2006.
Vandenberg AFB Vandenberg
AFB, California
U.S. Air Force Launch pads, vehicle assembly and
processing buildings, payload
processing facilities, telemetry and
tracking facilities, control center
engineering, user office space, and
Shuttle-capable runways.
Site is operational.
Wallops Flight
Facility
Wallops Island,
Virginia
NASA Telemetry and tracking facilities,
heavy jet-capable runway, launch
pads, vehicle assembly and
processing buildings, payload
processing facilities, mobile liquid
fueling facility under development
range control center, blockhouses,
large aircraft hangars, and user
office and lab space.
Final certification of the Wallops Mobile Liquid
Fueling Facility will be completed. Continued
development of Payload Processing Facility
High Bay is planned. Upgrades to MARS Pad 0-
B to accommodate larger vehicles is under
consideration.
White Sands
Missile Range
White Sands,
New Mexico
U.S. Army Full telemetry and tracking facilities,
runway engine and propulsion
testing facilities, class-100 clean
room for spacecraft parts.
Site is operational.
Table 4: Federal Spaceports Infrastructure and Status
Edwards completed an environmental assess-
ment for reentry corridors to EAFB for lifting entry
vehicles like the X-38 configuration.132 An addition-
al environmental assessment is being developed for
corridors that will allow flight tests within the
atmosphere for ranges of 741 kilometers (400 nauti-
cal miles) and 1,528 kilometers (825 nautical
miles).
NASA Kennedy Space Center
Established as NASA’s Launch Operations
Center in July 1962, Kennedy Space Center today
serves as the primary launch site for NASA’s
manned space missions. Major KSC facilities
include Launch Complex 39, supporting Space
Shuttle operations; the Vehicle Assembly Building
(VAB), where the Shuttle is integrated; and the
Shuttle Landing Facility. NASA KSC provides
oversight of NASA’s expendable launch vehicles
that are flown primarily from CCAFS and VAFB
with support from the USAF.
In September 2006, NASA KSC issued a
Request for Proposals (RFP) for the selection of a
master developer for a 129-hectare (319-acre) tech-
nology and commerce park at Kennedy Space
Center. The Exploration Park will be established to
enable and grow private sector participation in
space exploration, support commercial space trans-
portation, and promote commercial development of
technologies for application in space and on
Earth.133
Non-NASA use of KSC’s Shuttle Landing
Facility (SLF) increased during the last couple of
years. In January 2006, the SLF was used by the
GlobalFlyer airplane for a successful attempt to set
a new world record for the longest flight made by
any aircraft.134 NASA and ZERO-G signed an
agreement in April 2006 that will allow ZERO-G to
conduct up to 280 weightless flights annually in its
modified Boeing 727-200 aircraft from the SLF.135
In September 2006, NASA issued a request for
information from prospective commercial and other
non-NASA users of the SLF to support an environ-
mental assessment of commercial suborbital and
orbital spaceflight, support, and special purpose
aviation, and other compatible uses of the SLF. In
2007 NASA and Starfighters Inc. signed a coopera-
tive Space Act Agreement to enable the company’s
F-104 aircraft to fly simulated suborbital flight mis-
sions from the spaceport’s space shuttle runway.
The purpose of these flights is to gather data to sup-
port NASA’s assessment of expanding uses of the
SLF. The first in this series of pathfinder test mis-
sions took place in April 2007 and the flights gener-
ated “test data to validate sonic boom assumptions
about the potential impacts of suborbital and orbital
commercial spaceflight from the SLF. NASA is
assessing the environmental impact of such
flights.”137
Reagan Test Site
Located at Kwajalein Atoll, part of the
Republic of the Marshall Islands, the U.S. Army’s
Reagan Test Site (RTS) is part of the DoD Major
Range and Test Facility Base (MRTFB). The
advantages of RTS include its strategic geographi-
cal location, allowing launch in virtually all
Federal Aviation Administration Office of Commercial Space Transportation 57
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Shuttle landing at Edwards Air Force Base
KSC launches Space Shuttle Discovery
azimuths; unique instrumentation; and ability to
support ballistic missile testing and space opera-
tions. RTS is completely instrumented to support
space launch customers with radar, telemetry,
optics, and range safety systems. As a U.S. Army
DoD MRTFB, RTS receives annual federal funding
in addition to direct cost reimbursement from cus-
tomers.
A new launch pad on Omelek Island was con-
structed in 2006 to support space launch missions.
The Army began deployment of a fiber optic com-
munications system to the continental United
States, to be completed in late 2009, along with a
Huntsville, Alabama, Mission Control Center that
supports net-centric distributed operations.138
With nearly 40 years of successful support,
RTS provides a vital role in the research, develop-
ment, test and evaluation effort of America’s mis-
sile defense and space programs. At least 17 organi-
zations, representing the military, academia, civil
government, and commercial interests, use RTS.139
Among the users, there are U.S. Army, Navy, Air
Force, NSA, DOE, NRO, DARPA, Orbital
Sciences, and SpaceX. The SpaceX launches of
March 2006 and March 2007 were successfully
supported at RTS, although payloads did not reach
orbit. A Pegasus XL launch is scheduled from
Kwajalein in 2008.
Vandenberg Air Force Base
In 1941, the U.S. Army activated this site near
Lompoc, California, as Camp Cook. In 1957, Camp
Cook was transferred to the Air Force, becoming
the nation’s first space and ballistic missile opera-
tions and training base. In 1958, it was renamed in
honor of General Hoyt S. Vandenberg, the Air
Force’s second Chief of Staff. VAFB is currently
the headquarters of the 30th Space Wing and the
Air Force Space Command organization responsi-
ble for all DoD space and ballistic activities for the
West Coast. The 30th Space Wing Western Range
Operations Control Center provides flight safety,
weather, scheduling, instrumentation control, vehi-
cle designation information, and tracking data to
and from inter- and intra-range sensors in real or
nearly real-time for ballistic and space launch sup-
port. Range tracking capabilities extend over the
Pacific Ocean as far west as the Marshall Islands.
Boundaries to the north stretch as far as Alaska and
as far south as Central America. Vandenberg is host
to the 14th Air Force Headquarters and the Joint
Functional Component Command. Space infrastruc-
ture used for space launches at VAFB includes a
4,500-meter (15,000-foot) runway; boat dock; rail
lines; launch, booster, and payload processing facil-
ities; tracking radar; optical tracking and telemetry
facilities; and control centers. The 400-square-kilo-
meter (155-square-mile)
base also houses numerous
government organizations
and contractor companies.
VAFB hosts a variety of
federal agencies and attracts
commercial aerospace com-
panies and activities, includ-
ing the California Spaceport
effort. The 30th Space Wing
supports West Coast launch
activities for the USAF,
DoD, NASA, MDA and
various private industry
contractors. VAFB is
upgrading its range instru-
mentation and control cen-
ters to support the space
launch industry. Scheduled
for completion by 2010,
these upgrades will auto-
mate the Western Range and
provide updated services to
the customer. For the devel-
opment of launch infrastruc-
ture for the EELV program,
VAFB has partnered with
Boeing and Lockheed
Martin.
58 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Interceptor launched from Meck2 at Reagan Test Site
Delta II preparing forlaunch at VAFB
Boeing has renovated Space Launch Complex
6 (SLC-6) from a Space Shuttle launch pad into an
operational facility for Delta IV. Construction at
SLC-6 has included enlarging the existing mobile
service tower and completing the construction of
the West Coast Horizontal Integration Facility,
where the Delta IV is assembled.
Lockheed Martin converted SLC-3E from an
Atlas 2 launch pad into an operational facility for
Atlas V. The upgrades started in January 2004,
which include adding 9 meters (30 feet) to the
existing 61-meter (200-foot) mobile service tower
to accommodate the larger rocket. A crane capable
of lifting 20 tons was replaced with one that can lift
60 tons. Current space launch vehicles supported by
VAFB include Delta II, Delta IV, Atlas V, Taurus,
Minotaur, Pegasus XL, and Falcon 1. During 2007,
VAFB supported three Delta II launches and one
Pegasus XL launch. Orbital Sciences’ Taurus is
launched from 576E. Pegasus XL vehicles are
processed at Orbital Sciences’ facility at VAFB then
flown to various worldwide launch areas.
Vandenberg supports numerous ballistic programs,
including Minuteman and numerous MDA test and
operational programs. SpaceX maintains a launch
pad at SLC-3 West for its Falcon 1 rocket, and
plans future developments for its larger Falcon 9
rocket for sending commercial and government
payloads into polar and other high inclination
orbits.
Vandenberg Air Force Base has active part-
nerships with private commercial space organiza-
tions in which VAFB provides launch property and
launch services. The private companies use the gov-
ernment or commercial facilities to conduct launch,
payload, and booster processing work. VAFB hous-
es three commercially owned complexes: Boeing’s
Horizontal Integration Facility, Spaceport Systems
International’s (SSI) California Spaceport and
Payload Processing Facility, and Astrotech’s
Payload Processing Facility.140
Wallops Flight Facility
The predecessor of NASA, the National
Advisory Committee for Aeronautics, (NACA),
established an aeronautical and rocket test range at
Wallops Island, Virginia, in 1945. Since then, over
15,000 rocket launches have taken place from the
Wallops Flight Facility (WFF), which is operated
for NASA by the Goddard Space Flight Center,
Greenbelt, Maryland.
WFF’s primary mission is to serve as a
research and test range for NASA, supporting sci-
entific research, technology development, flight
testing, and educational flight projects. WFF, how-
ever, also heavily supports the DoD and commer-
cial industry with flight projects ranging from small
suborbital vehicles to orbital launch vehicles. In
addition to rockets, WFF’s integrated Launch
Range and Research Airport enables flight opera-
tions of UAVs and other experimental craft. WFF
frequently serves as a downrange site for launches
conducted from Cape Canaveral.
MARS is co-located at WFF as a tenant, and
the organizations collaborate on certain projects to
provide mission services, particularly focusing on
small commercial ELVs. Jointly, WFF and MARS
offer two orbital and several suborbital launchers, a
range control center, three blockhouses, numerous
payload and vehicle preparation facilities, and a full
suite of tracking and data systems. In support of its
research and program management responsibilities,
Wallops also contains numerous science facilities, a
research airport, and flight hardware fabrication and
test facilities.
WFF has continued a significant range mod-
ernization and technology program that began in
2002. WFF engineers are also actively pursuing
new range technologies that will increase respon-
siveness and lower costs, such as space-based com-
munications systems and an autonomous flight ter-
mination system.141 The Payload Processing Facility
is operational and being used. The class-100,000
certification testing for the entire facility is pending,
Federal Aviation Administration Office of Commercial Space Transportation 59
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Wallops Flight Facility
as only half the facility obtained this certification.
The new project support facility, providing auditori-
um capabilities for large gatherings, including pre-
mission reviews and observation of the launch, was
completed in 2007.142 The new engineering facility
hosting WFF engineering staff and laboratories was
also finished in 2007.143 Final certification of the
Wallops Mobile Liquid Fueling Facility is still to be
completed. Future plans include a barge dock
improvement to enable water transport between the
Mainbase and the Island campuses.
During 2006, WFF’s Research Range support-
ed 30 rocket tests. WFF is heavily engaged in sup-
porting both DoD and commercial interests in the
emerging small ELV community, such as those sup-
ported by the DARPA Falcon program. During
2007, twelve suborbital and orbital rocket tests
were conducted from WFF. WFF supported MARS
with two orbital missions: the launch of the USAF
and NASA TacSat 2 satellite in December 2006,
and the NFIRE satellite in April 2007, each using a
Minotaur I.
White Sands Missile Range
Once exclusively military, White Sands
Missile Range (WSMR) today attracts other gov-
ernment agencies, foreign nations, and private
industry to its world-class test facilities. The largest
overland test range in America, WSMR is operated
by the U.S. Army and used by the Army, Navy, Air
Force, Marine Corps, and MDA. It is also home to
the NASA White Sands Test Facility. Situated 26
kilometers (16 miles) northeast of Las Cruces, New
Mexico, this range covers 8,100 square kilometers
(3,127 square miles).
Since establishment in 1945, the range has
fired more than 44,500 missiles and rockets. Almost
1,200 of those were research and sounding rockets.
WSMR has seven engine test stands and precision
cleaning facilities, including a class-100 clean room
for spacecraft parts. After KSC and EAFB, White
Sands is the Space Shuttle’s tertiary landing site.
This landing site consists of two 11-kilometer (6.8
mile) long gypsum-sand runways.144 Test operations
are run out of the new J.W. Cox Range Control
Center. This $28-million facility was designed to
meet current and future mission requirements with
state-of-the-art networking, computing, and com-
munications for effective interaction between test
operations and customers.
In 2002, the U.S. Army, WSMR, and state of
New Mexico signed a Memorandum of Agreement
supporting the development of the Southwest
Regional Spaceport, which was renamed Spaceport
America in 2006. WSMR provided range support
for the first suborbital rocket launch from Spaceport
America in October 2006. WSMR provided track-
ing, communication and other services to support
the suborbital space launch conducted by UP
Aerospace in April, 2007.145 Initially WSMR will
provide a diversity of support services for
Spaceport America, including flight safety, radar,
optical tracking, and airspace and ground space for
touchdown and recovery.
Proposed Non-Federal Spaceports
Several states plan to develop spaceports
offering a variety of launch and landing services.
Two common characteristics of many of the pro-
posed spaceports are inland geography – a contrast
to the coastal location of all but two present-day
U.S. spaceports – and interest in hosting RLV oper-
ations. Table 5 describes specific efforts to establish
non-federal spaceports, which are in various stages
of development.
Cecil Field Spaceport
Originally developed as a Naval Air Station
with one 3,810-meter (12,500-foot) runway and one
1,160-meter (3,800-foot) runway, Cecil Field was
proposed for closure by the Base Realignment and
Closure (BRAC) process in 1993. Five years later,
based on the recommendation of the Base Reuse
Commission, Jacksonville Aviation Authority
(JAA) took ownership of 3,240 hectares (8,000
60 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
White Sands Missile range
Federal Aviation Administration Office of Commercial Space Transportation 61
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Table 5: Proposed Non-federal Spaceports Infrastructure and Status
Spaceport Location Owner/Operator Launch Infrastructure Development Status
Cecil Field
Spaceport
Jacksonville,
Florida
Jacksonville Aviation
Authority
One 3,810-m (12,500-ft) runway, three
2,440-m (8,000-ft) runways, 175
buildings totaling 270,000-m2 (2.9 million-
ft2), 8 aircraft hangars, operating air
traffic control tower, warehouse,
industrial and general use space totaling
more than 40,000-m2 (425,000-ft2) and
general office and support facilities of
over 21,000-m2 (225,000-ft2).
The environmental assessment for spaceport
operations was completed in 2007. FAA
reviewed it and instructed JAA to initiate the
launch site operator's licensing process.
Discussions are currently underway to establish
Airspace Agreements with FAA and the U.S.
Navy. The Jacksonville Aviation Authority
expects to submit an application for a launch
site operator license in 2008.
Chugwater
Spaceport
Platte County,
Wyoming
Frontier Astronautics No complete infrastructure at this time. Three launch pads and a 2,225,000-n (500,000-
ft·lbf) flame trench are being refurbished.
Environmental assessment for site approval is in
progress and expected to be completed in 2008.
South
Texas
Spaceport
Willacy
County, Texas
Willacy County
Development
Corporation for
Spaceport Facilities
Road, as an extension to the road to the
airport, 6-in water line with fire hydrant,
18 x 25 x 5-m (60 x 80 x 16-ft) metal
building with concrete slab.
The final Texas Spaceport site is in Port
Mansfield, near Charles R. Johnson Airport. The
interior of the building was finished in 2007.
Spaceport
Alabama
Baldwin
County,
Alabama
To be determined No infrastructure at this time. The master plan Phase 1 has been completed
and Phase 2 is under development. While no
land has been acquired for Spaceport Alabama,
a green field site is under consideration in
Baldwin County, across the bay from the city of
Mobile.
Spaceport
America
Upham, New
Mexico
New Mexico
Spaceport Authority
Major components of the proposed
Spaceport America include two launch
complexes, a landing strip, an aviation
complex, and support facilities.
Plans for this site include a spaceport central
control facility, an airfield, a maintenance and
integration facility, a launch and recovery
complex, a flight operations control center, and a
cryogenic plant. Construction to begin in third
quarter of 2007. Environmental and business
development studies conducted. First suborbital
launch took place in September 2006, with
another one following in April 2007.
Spaceport
Sheboygan
Sheboygan,
Wisconsin
Owner: City of
Sheboygan; Operator:
Rockets for Schools
A vertical pad for suborbital launches in
addition to portable launch facilities,
such as mission control.
Plans for developing additional launch
infrastructure are ongoing and include creation
of a development plan that includes support for
orbital RLV operations. Wisconsin Aerospace
Authority legislation was signed into law in 2006.
Spaceport
Washington
Grant County
International
Airport,
Washington
Port of Moses Lake 4,100-m (13,452-ft) main runway and a
3,200-m (10,500-ft) crosswind runway.
A 12,100 ha (30,000-a) potential vertical launch
site has been identified. An Aerospace Overlay
Zone has also been established in the Grant
County Unified Development Code. The site is
certified as an emergency-landing site for the
Space Shuttle. Additional infrastructure
development is pending launch customers and
market responses.
West Texas
Spaceport
Pecos County,
Texas
Pecos County/West
Texas Spaceport
Development
Corporation
Greasewood site has an air conditioned
control center, an industrial strength
concrete pad, and a 30 x 30-m (100 x
100-ft) scraped and level staging area.
Broadband Internet on site, controlled
fenced access, and a 1,295-km2 (500
mi2) recovery area. Airport has 5
runways (2,286 x 30-m, or 7,500 x 100-
ft) with hangar space.
Development plan approved by State of Texas in
2005. State has provided $175,000 in 2005 for
planning studies. Future infrastructure plans
include 1,070-m (3,500-ft) runway, static engine
testing facility, and balloon hangar.
62 Federal Aviation Administration Office of Commercial Space Transportation
acres), including the runways, hangars, and support
infrastructure, and has operated the airport for
maintenance and repair operations, general aviation
activity, and limited military operations. The airport
was identified as a potential launch site in the feasi-
bility study of a Florida commercial spaceport.
Space Florida has been instrumental in providing
guidance and direction for the development of the
Cecil Field Spaceport.146 The JAA is pursuing a
launch site operator’s license. The environmental
assessment needed for the issuance of the license
was completed in 2007. The JAA expects to submit
an application for a launch site operator license in
2008.
The existing infrastructure of this airfield is
conducive to spaceport operations, including one
3,810-meter (12,500-foot) runway, three 2,440-
meter (8,000-foot) runways, 175 buildings totaling
270,000 square meters (2.9 million square feet),
eight aircraft hangars, an operating air traffic con-
trol tower, warehouse, industrial and general use
space totaling more than 40,000 square meters
(425,000 square feet), and general office and sup-
port facilities of over 21,000 square meters
(225,000 square feet). The long runway, together
with its location in a sparsely populated area and
the proximity to the coast, make this site attractive
for future commercial space activities. During
2007, JAA performed roof rehabilitation on six
hangars and the terminal, structural upgrades and
renovation of the air traffic control tower, and
development of a new taxiway and an approach
lighting system. JAA also conducted rehabilitation
of the airfield
electrical sys-
tem, security
fencing, and air-
field pavement,
as well as
improvement in
the stormwater
drainage and fire
suppression
waterline. The
construction and
rehabilitation
work JAA com-
pleted required
an investment of
over $9 million
that came from FAA Discretionary Funds and
Annual General Aviation Entitlements, as well as
from the Florida Department of Transportation and
JAA.
The plan is for Cecil Field Spaceport to use
facilities that currently exist at the site. Future
infrastructure planned for the facility includes pave-
ment, fencing, stormwater plan, parking, access
road improvements, and design and construction of
an additional apron and of two additional hangars,
each of 14,000 square meters (150,000 square feet).
The hangars are scheduled for completion in 2008.
The proposed spaceport operations, including hori-
zontal launches and launch recoveries, will be con-
ducted using Runway 18L/36R, which measures
3,810 meters (12,500 feet) in length and 60 meters
(200 feet) in width.147
An official development plan focusing solely
on the economic growth and operation of the Cecil
Field Spaceport is currently being considered for
development. The Cecil Field Airport Master Plan
and Airport Layout Plan Update were completed in
September 2007. These documents are currently
under review by FAA, FDOT, and the City of
Jacksonville, Florida.
Chugwater Spaceport
The Chugwater Spaceport was originally an
Atlas E missile base outside of Chugwater,
Wyoming, built in 1960 and decommissioned in
1965. Designed to store and launch a complete
Atlas E ICBM, the facilities are designed with
many special amenities for rocketry. In March
2006, Frontier Astronautics bought the property and
began renovation to use it as a launch site.
Since the last change in ownership, mainte-
nance work has been performed to get original mili-
tary equipment operational. During 2006, three hor-
izontal engine tests of a LOX and kerosene Viper
33,360-newton (7,500-pound-force) engine took
place at the Chugwater site. During 2007, several
dozen test firings of rocket engines have occurred,
as well as a completed flight vehicle test (the
SpeedUp Laramie Rose Lunar Lander Challenge
vehicle). All of these have taken place over the
instrumented flame trench. The tests were possible
because Frontier Astronautics obtained an exception
to a countywide fire ban.
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Cecil Field Aerial View
So far, almost $600,000 has been invested in
the site, all from private sources. The environmen-
tal assessment is expected to be completed in 2008
and Chugwater Spaceport will apply for an FAA
license in 2008. No direct financial support is
expected from the state. In 2007 X-L Space
Systems has set up facilities in the spaceport and
has started producing rocket-grade hydrogen perox-
ide for sale to other space companies. Plans for
future infrastructure include a functioning
2,225,000-newton (500,000-pound-force) vertical
test stand for engine testing, up to three vertical
launch pads, on-site machine shop, and shooting
range. An additional horizontal engine test area is
in development. The planned configuration of the
spaceport launch site is vertical launch pads with
water acoustic suppression system.148
South Texas Spaceport
Willacy County Development Corporation
was created in 2001 to manage the spaceport site
evaluation and other technical and administrative
elements of the project under a Texas Aerospace
Commission grant. Willacy County Development
Corporation for Spaceport Facilities is the owner of
the spaceport.
The designated spaceport site is a 40.5-
hectare (100 acre) undeveloped site in Port
Mansfield, adjacent to the Charles R. Johnson
Airport, approximately 150 kilometers (93 miles)
south of Corpus Christi and 65 kilometers (40
miles) north of Brownsville. The site initially may
support the suborbital and small orbital launch sys-
tems currently in service or being developed for
service in the near future, with a long-term focus on
RLVs. All launches will be from spoil islands or
barges in the Mansfield ship channel in the Laguna
Madre or Gulf of Mexico.
During 2006, almost $200,000, including in-
kind contributions, was invested in building new
infrastructure. All the new developments in 2006
happened with the assistance of government fund-
ing. Preliminary spaceport construction was com-
pleted. A new road was installed, an extension to
the road to the airport. A 15-centimeter (6-inch)
water line with fire hydrant was added to the new
18 x 25 x 5 meter (60 x 80 x 16 feet) metal build-
ing with concrete slab. During 2007, the interior of
the building with offices and bathrooms was com-
pleted. The State of Texas financed these efforts,
which totaled to approximately $25,000. The
launch barge for all launches still needs to be pur-
chased.
Spaceport Alabama
Proposed as a next-generation spaceport,
Spaceport Alabama will be a full-service departure
and return facility, supporting orbital and suborbital
space access vehicles. Spaceport Alabama is in the
planning phase under direction of the Spaceport
Alabama Program Office at Jacksonville State
University in Alabama. Phase 1 of the Spaceport
Alabama master planning process is now complete,
and phase 2 has commenced. Upon completion of
the Spaceport Alabama master plan, a proposal will
be presented to the Alabama Commission on
Aerospace Science and Industry and the Alabama
Legislature for formal adoption. Under the current
plan, the Alabama Legislature would establish the
Spaceport Alabama Authority, which would oversee
development of Spaceport Alabama. While no land
has been acquired for Spaceport Alabama, a green
field site is under consideration in Baldwin County,
across the bay from the city of Mobile. This site is
seen as ideal for supporting government and com-
mercial customers, operating next-generation
reusable flight vehicles that are designed for access
to LEO, MEO (medium Earth orbit), and GEO.149
Under the current spaceport development
plan, a spaceport facility could become operational
within 10 years, depending on market demand. This
Federal Aviation Administration Office of Commercial Space Transportation 63
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Chugwater Aerial View
plan calls for the establishment of a “total spaceport
enterprise” concept, consisting of a departure and
return facility, processing and support facilities, and
full support infrastructure. An R&D park, a com-
merce park, supporting community infrastructure,
intermodal connectivity, and other services and
infrastructure necessary for providing a turnkey
capability in support of space commerce, R&D,
national security, science, and related services are
also included in this plan. Given that the site cur-
rently under consideration is adjacent to the Gulf of
Mexico, Spaceport Alabama would service primari-
ly RLVs; however, some suborbital ELVs involving
scientific and academic missions could be support-
ed. The spaceport hopes to continue development as
industry opportunities emerge.
Spaceport America
The state of New Mexico continues to make
significant progress in the development of
Spaceport America, known as Southwest Regional
Spaceport prior to July 2006. In December 2005,
Richard Branson decided to establish the headquar-
ters of Virgin Galactic in New Mexico and use
Spaceport America as its primary operating base.
He also entered into a partnership with the state of
New Mexico to build the spaceport. While the state
would build the spaceport, Virgin Galactic would
sign a 20-year lease agreement with annual pay-
ments of $1 million for the first 5 years. The state
government would pay about half of the construc-
tion cost, with the difference to come from local
and federal governments.150 The spaceport is
planned to receive $140 million as direct financial
support from the state and $58 million as direct
financial support from local government, beginning
with 2008.151
Spaceport America is being developed for use
by private companies and government organizations
conducting space activities and operations. In
March 2006, New Mexico passed a bill that created
one entity, New Mexico Spaceport Authority, to
oversee the spaceport. Spaceport America is cur-
rently taking steps to obtain an FAA launch site
operator license. The state owns and operates the
spaceport and will lease the facilities to the users.
Currently, agreements are being developed with dif-
ferent organizations.152 In January 2006, New
Mexico state officials signed an agreement that
gives the planned spaceport north of Las Cruces
access to nearly 6,070 hectares (15,000 acres) of
state trust land to begin developing the site.153 The
spaceport is a 70-square-kilometer (27- square-
mile) parcel of open land in the south central part
of the state, near the desert town of Upham, 72
kilometers (45 miles) north of Las Cruces and 48
kilometers (30 miles) east of Truth or
Consequences, at approximately 1,430 meters
(4,700 feet) above sea level. This location was
selected for its low population density, uncongested
airspace, and high elevation.154
During 2006, temporary facilities added to the
site include a launch pad, a weather station, rocket
motor storage facilities, and trailers. This infrastruc-
ture is worth $450,000; the funding came from pri-
vate and government sources. Major components of
the proposed Spaceport America include two launch
complexes, a landing strip, an aviation complex,
and support facilities. The spaceport has an official-
ly approved development plan that includes begin-
ning construction in third quarter of 2008, and hav-
ing a full-fledged spaceport to support vertical
launches, vertical landings, and horizontal landings
by 2010.155 Currently, DMJM/AECOM, an architec-
ture and engineering contractor, is designing the
facilities with inputs from the spaceport users, as
the final configuration will be customer driven.
New Mexico provides several tax and busi-
ness incentives for the spaceport-related industrial
activities, including gross receipt deductions,
exemptions from compensating taxes, R&D incen-
tives, industrial revenue bonds, and investment and
job training credits. The state has also passed legis-
lation that allows counties and municipalities to
impose, upon voter approval, a regional spaceport
gross receipt tax in increments of one-sixteenth per-
cent, not to exceed one-half percent.156
64 Federal Aviation Administration Office of Commercial Space Transportation
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
Cutaway View of Spaceport America facility
The first launch from the spaceport took place
on September 25, 2006, when UP Aerospace
launched an amateur-class vehicle. On April 28,
2007 UP Aerospace launched another amateur-class
vehicle, SL-2. The commitment in building the
spaceport, the recent activities there, and state
incentives to locate space-related businesses in New
Mexico have made the state an attractive location
for rocket activity, such as Starchaser Industries, the
X PRIZE Cup, and the Rocket Racing League.
Spaceport Sheboygan
On August 29, 2000, the Wisconsin
Department of Transportation officially approved
creating the Spaceport Sheboygan, located on Lake
Michigan in Sheboygan, Wisconsin. The city of
Sheboygan owns the spaceport, which strives to
support space research and education through sub-
orbital launches for student projects.
Suborbital sounding rocket launches to alti-
tudes of up to 55 kilometers (34 miles) have been
conducted at the site. Additionally, Rockets for
Schools, a student program founded in Wisconsin
by Space Explorers, Incorporated, and developed
by the Aerospace States Association, has conducted
suborbital launches at Spaceport Sheboygan since
its inception in 1995. Each year, hundreds of stu-
dents from Wisconsin, Illinois, Iowa, and Michigan
participate in these launches, which took place most
recently in May 2007. Rockets for Schools is a pro-
gram of the Great Lakes Spaceport Education
Foundation.
The spaceport’s existing infrastructure
includes a vertical pad for suborbital launches in
addition to portable launch facilities, such as mis-
sion control, which are erected and disassembled as
needed. The pier, which the city leased from the
U.S. Army Corps of Engineers for spaceport
launches and citizens’ enjoyment (i.e., walking and
fishing), was widened and strengthened in 2004. In
May 2007, under the Rockets for Schools program,
more than 45 rockets were launched off of the pier.
In 2006 some structures were removed to clear
space for the construction of a proposed mission
control and education center. Past construction has
been financed through municipal, state, and federal
agencies. The State of Wisconsin contributed to the
development of the spaceport with site preparation
of coastline and access roads. No new infrastructure
was constructed during 2007.
Legislation for the creation of the Wisconsin
Aerospace Authority (WAA) was signed into law in
2006. WAA will meet for the first time in January
2008. WAA will design, develop, and operate the
spaceport. The board was created to market the
state to the aerospace industry, develop space-relat-
ed tourism, and work with educators to promote
math and science classes with a greater focus on
aeronautics and engineering.157 The legislation
authorizes the WAA to develop spaceports, space-
craft, and other aerospace facilities in Wisconsin;
provide spaceport and aerospace services; allow use
of spaceport and aerospace facilities by others; pro-
mote the aerospace industry in Wisconsin; and pro-
vide public-private coordination for the aerospace
industry in Wisconsin.158 In addition to designing,
developing, and operating the spaceport, WAA is
authorized to sell up to $100 million in revenue
bonds.159
The spaceport establishment project has sev-
eral phases. The first phase refers to the develop-
ment of the Great Lakes Aerospace Science and
Education Center at Spaceport Sheboygan and is
currently underway. A preliminary business plan for
the center has already been developed. The second
Federal Aviation Administration Office of Commercial Space Transportation 65
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Rocket launch from Spaceport Sheboygan
phase for the project includes proposing legislation
for the development and operational plans of the
Spaceport Sheboygan. Once the legislation is
approved, WAA will conduct site evaluation, feasi-
bility, and environmental impact studies. Project
supporters are in the initial stages of obtaining an
FAA launch site license.160 Future projects include
adding orbital launch capabilities for RLVs, includ-
ing a horizontal and vertical launch site.
Spaceport Washington
Spaceport Washington, a public and private
partnership, has identified Grant County
International Airport in central Washington, 280
kilometers (174 miles) east of Seattle, as the site of
a future spaceport. The airport (formerly Larson Air
Force Base and now owned and operated by the
Port of Moses Lake) is used primarily as a testing
and training facility. Spaceport Washington propos-
es to use Grant County International Airport for
horizontal and vertical take-offs and horizontal
landings of all classes of RLVs. This airport has a
4,100-meter (13,452-foot) main runway and a
3,200-meter (10,500-foot) crosswind runway and is
certified as an emergency landing site for the Space
Shuttle. The spaceport does not have an official
development plan yet, but the intended configura-
tion of the spaceport launch site will either be verti-
cal launch and horizontal recovery or horizontal
launch and recovery.161
An approximately 121-square-kilometer
(30,000-acre) potential vertical launch site has been
identified with multiple owners (both public and
private). The spaceport has also established an
Aerospace Overlay Zone within the Grant County
Unified Development Code. This zone protects the
air and land space around the area proposed for use
as an aerospace launch and retrieval facility from
obstructions or hazards and incompatible land uses
in the proximity of the Grant County International
Airport. Additional infrastructure development
depends on launch customers’ needs and market
responses.162 At present, Spaceport Washington is
seeking launch operators. It will not apply for an
FAA launch license until it has viable operations
and a business plan.163
West Texas Spaceport
The Pecos County/West Texas Spaceport
Development Corporation, established in mid-2001,
is moving forward with the development of a
spaceport 29 kilometers (18 miles) southwest of
Fort Stockton, Texas. Spaceport infrastructure will
include a launch site with a 4,570-meter (15,000-
foot) safety radius, an adjacent recovery zone (193
square kilometers or 500 square miles), payload
integration and launch control facilities, and the
Pecos County Airport runway (2,310-meters or
7,500 feet) and hangar complex. The site has access
to over 1,740 square kilometers (4,500 square
miles) of unpopulated land and over 3,860 square
kilometers (10,000 square miles) of underutilized
national airspace. The West Texas Spaceport is
mainly an R&D site for UAVs and suborbital rock-
ets. The primary users of this spaceport currently
are operators of unmanned air systems.
A joint project with the school district has
made a technology center available for Pecos
County Aerospace Development Center users. The
Technology Center has multiple monitors, high-
speed Internet service, and full multiplexing capa-
bility. The Pecos County/West Texas Spaceport
Development Corporation has access to optical
tracking and high-speed video capability that can
record a vehicle’s flight up to tens of thousands of
feet (depending upon the size of the vehicle)
regardless of its speed.164 For the past two years,
Pecos County/West Texas Spaceport Development
Corporation has been involved in educational activ-
ities, under the framework of Texas Partnership for
Aerospace Education, to promote and support aca-
demic programs in aero-science and rocketry.
Spaceports 2008 U.S. Commercial Space Transportation Developments and Concepts
66 Federal Aviation Administration Office of Commercial Space Transportation
Spaceport Washington Aerial View
Future infrastructure plans include the devel-
opment of a privately-funded 1,077-meter (3,500-
foot) runway, a static engine test facility, and a
hangar for balloon and wind sensitive activities.
Other projects pursued by the Pecos County/West
Texas Spaceport Development Corporation include
the Blacksky DART program, intended to charac-
terize the performance of an innovative aerospike
nozzle on a solid rocket motor.165
2008 U.S. Commercial Space Transportation Developments and Concepts Spaceports
Federal Aviation Administration Office of Commercial Space Transportation 67
Regulatory Developments 2008 U.S. Commercial Space Transportation Developments and Concepts
68 Federal Aviation Administration Office of Commercial Space Transportation
In 2007, the FAA continued to enhance and refine
its regulations in three primary areas—private
human spaceflight, experimental launches, and
amateur rockets—in ways that balanced promotion
of a vigorous U.S. commercial space industry with
the need to safeguard the public. This section
reviews the most recent regulatory developments in
these three areas. As this section is a summary, the
FAA recommends that readers interested in further
details consult the regulatory documents in their
entirety, available online at http://ast.faa.gov.
Private Human Space Flight
On December 23, 2004, the President signed
into law the Commercial Space Launch Amendments
Act of 2004 (CSLAA). The CSLAA promotes the
development of the emerging commercial space
flight industry and makes the Federal Aviation
Administration (FAA) responsible for regulating
commercial human space flight. Recognizing that
this is a fledgling industry, the law required a
phased approach in regulating commercial human
space flight, with regulatory standards evolving as
the industry matures.
On December 15, 2006, the FAA issued regu-
lations establishing requirements for crew and
space flight participants involved in private human
space flight. The new rules, which became effective
on February 13, 2007, maintain FAA’s commitment
to protect the safety of the uninvolved public and
call for measures that enable space flight partici-
pants to make informed decisions about their per-
sonal safety. The CSLAA characterizes what is
commonly referred to as a passenger as a “space
flight participant.” The statute defines this person to
mean “an individual, who is not crew, carried with-
in a launch or reentry vehicle.” This characteriza-
tion signifies that someone on board a launch or
reentry vehicle is not a typical passenger with typi-
cal expectations of transport, but instead someone
going on an adventure ride.
The regulations require launch vehicle opera-
tors to provide certain safety-related information
and identify what an operator must do to conduct a
licensed launch with a human on board. In addition,
launch operators must inform passengers of the
risks of space travel generally and the risks of space
travel in the operator’s vehicle in particular. These
regulations also include training and general securi-
ty requirements for space flight participants.
The regulations also establish requirements
for crew notification, medical qualifications and
training, and requirements governing environmental
control and life support systems. In particular, the
regulations require a pilot of a launch or reentry
vehicle to possess and carry an FAA pilot certificate
with an instrument rating. Each crew member with
a safety-critical role must possess and carry an FAA
second-class airman medical certificate. The regula-
tions require an operator to verify the integrated
performance of a vehicle’s hardware and any soft-
ware in an operational flight environment before
allowing any space flight participant on board.
Verification must include flight testing.
Since the human space flight regulations were
issued, the FAA has begun to develop advisory cir-
culars or guidance documents in the areas of human
space flight crew training and environmental con-
trol and life support systems (ECLSS) for subor-
bital missions. These documents will provide guid-
ance and acceptable means of meeting some of the
human space flight regulations pertaining to crew
training and ECLSS.
Finally, the regulations establish financial
responsibility and waiver of liability requirements
to human space flight and experimental permits in
accordance with the CSLAA. The CSLAA requires
crew and space flight participants to enter into a
reciprocal waiver of claims with the U.S. govern-
ment. Furthermore, the CSLAA expressly excludes
space flight participants from eligibility for indem-
nification against third party claims. Launches and
reentries performed pursuant to a permit are also
excluded from eligibility for indemnification.
Experimental Launch Permits
A number of entrepreneurs are committed to
the goal of developing and operating reusable
launch vehicles for private human space travel. In
order to promote this emerging industry and to cre-
ate a clear legal, regulatory, and safety regime, the
Regulatory Developments
Regulatory Developments 2008 U.S. Commercial Space Transportation Developments and Concepts
69 Federal Aviation Administration Office of Commercial Space Transportation
2004 CSLAA also established an experimental per-
mit category for launching developmental reusable
suborbital rockets on suborbital trajectories.i The
FAA issued regulations implementing this alterna-
tive to a license on April 6, 2007. This section
details eligibility requirements for experimental
permits, notes how they differ from licenses, and
discusses how they are implemented and administered.
Eligibility
To be eligible for an experimental permit, an
applicant must propose to fly a reusable suborbital
rocket for the following purposes:
• Research and development to test new
design concepts, new equipment, or new
operating techniques;
• Demonstration of compliance with require
ments as part of the process for obtaining a
license; or
• Crew training before obtaining a license
for a launch or reentry using the design of
the rocket for which the permit would be
issued.
Experimental Permit Compared to a License
An experimental permit differs from a license
in several ways, including the following:
• The FAA must determine whether to issue
an experimental permit within 120 days of
receiving an application. For a license, it is
180 days.
• Under a permit, a reusable suborbital
rocket may not be operated to carry
property or human passengers for
compensation or hire. No such restriction
applies for a license.
• Damages arising from a permitted launch
or reentry are not eligible for “indemnifi-
cation,” the provisional payment of claims
under Chapter 701. Damages caused by
licensed activities, by contrast, are eligible
for the provisional payment of claims to
the extent provided in an appropriation law
or other legislative authority.
• A permit must authorize an unlimited
number of launches and reentries for a
particular reusable suborbital rocket
design. Although a license can be
struc-tured to authorize an unlimited
number of launches, no statutory mandate
to do so exists.
• Under a permit, a launch operator is not
required to demonstrate that the risk from a
launch falls below specified quantitative
criteria for collective and individual risk.
Under a license, a launch operator must.
• Under a permit, a launch operator is not
required to have a separate safety
organization or specific safety personnel.
Under a license, a launch operator must.
Safety Measures
The experimental permit regulations include a
variety of safety measures to protect the public.
The most important is an applicant-derived hazard
analysis. A hazard analysis is a system safety engi-
neering tool that identifies and characterizes haz-
ards and qualitatively assesses risks. An applicant
for a permit must perform a hazard analysis and
provide the results to the FAA. A permit applicant
uses this analysis to identify its risk elimination and
mitigation measures to reduce risk to an acceptable
level. An applicant must show that selected risk
elimination and mitigation measures will work.
Applicants may demonstrate this through providing
flight demonstration test data; component, system,
or subsystem test data; inspection results; or analysis.
Using the hazard analysis, most safety solu-
tions are derived by the launch operators them-
selves. The regulations do, however, contain a num-
i The CSLAA defines a suborbital rocket as a vehicle, rocket-propelled in whole or in part, intended for flight on a suborbital
trajectory, whose thrust is greater than its lift for the majority of the rocket-powered portion of ascent. A suborbital trajectory is
defined in the CSLAA as the intentional flight path of a launch vehicle, reentry vehicle, or any portion thereof, whose vacuum
instantaneous impact point does not leave the surface of the Earth.
Regulatory Developments 2008 U.S. Commercial Space Transportation Developments and Concepts
70 Federal Aviation Administration Office of Commercial Space Transportation
ber of operating requirements that the FAA believes
are too important to omit. These include:
• Rest rules for vehicle safety operations per
sonnel
• Pre-flight and post-flight operations
• Operating area containment
• Key flight-safety event limitations
• Landing and impact locations
• Agreements with other entities involved in
a launch or reentry
• Collision avoidance analysis
• Tracking a reusable suborbital rocket
• Communications
• Flight rules
• Anomaly recording and reporting
• Mishap reporting, responding, and investi
gating
Operating area containment, key flight safety
event limitations, and anomaly reporting are dis-
cussed below.
Operating Area Containment
Central to the experimental permit approach is
containment of the reusable suborbital rocket within
one or more defined operating areas. A permit
applicant must define an acceptable operating area,
and must demonstrate to the FAA that it can contain
its reusable suborbital rocket’s instantaneous impact
point (IIP)ii within the operating area and outside
any FAA-defined exclusion area.iii
An operating area is a three-dimensional
region meeting the following criteria:
• Must be large enough to contain each
planned trajectory and all expected vehicle
dispersions;
• Must contain enough unpopulated or
sparsely populated area to perform key
flight-safety events, discussed below;
• May not contain or be adjacent to a dense
ly populated area or large concentrations of
members of the public; and
• May not contain or be adjacent to signifi
cant automobile traffic, railway traffic, or
waterborne vessel traffic.
The above criteria are designed to prohibit the
operation of a reusable suborbital rocket over areas
where the consequences of an uncontrolled impact
of the vehicle or its debris would be catastrophic.
Note that agreements with FAA Air Traffic Control
would also influence the size and location of an
operating area. Although conditions on the ground
may be favorable for flight test, airspace concerns
may limit the feasibility of an otherwise acceptable
operating area.
During the application process, an applicant
must identify and describe the methods and systems
used to contain its reusable suborbital rocket’s IIP
within the operating area and outside any exclusion
area. Acceptable methods and systems would
include but not be limited to:
• Proof of physical limitations on a vehicle’s
ability to leave the operating area; and
• Abort procedures and safety measures
derived from a system safety process.
Proof of physical limitations on a vehicle’s
ability to leave the operating area could be obtained
through an analysis that showed that the maximum
achievable range of the reusable suborbital rocket
from the launch point was within the boundaries of
the operating area, assuming the rocket flew a tra-
ii An IIP is an impact point, following thrust termination of a launch vehicle, calculated in the absence of atmospheric drag
effects.iii An exclusion area is an FAA defined area on the ground that warrants special protection for safety or policy purposes.
Regulatory Developments 2008 U.S. Commercial Space Transportation Developments and Concepts
71 Federal Aviation Administration Office of Commercial Space Transportation
jectory optimized for range and that all safety sys-
tems failed.
An applicant could use its hazard analysis to
determine safety measures to keep a reusable subor-
bital rocket’s IIP within its operating area.
Alternatively, an applicant could perform a separate
and more comprehensive system safety analyses
solely for containment. Specific safety measures
obtained from a system safety process could
include a dedicated flight safety system or systems
and procedures that, while not dedicated exclusive-
ly to flight safety, help to protect the public.
Key Flight-Safety Event Limitations
Operating within an acceptable operating area
and implementing safety measures obtained from a
hazard analysis are only part of what would be nec-
essary to maintain public safety. Because of the
uncertainty in operating developmental reusable
suborbital rockets, a permittee must conduct “key
flight-safety events” over unpopulated or sparsely
populated areas. A key flight-safety event is a per-
mitted flight activity that has an increased likeli-
hood of causing a failure compared with other por-
tions of flight. Events such as rocket engine igni-
tion, staging, and envelope expansion have histori-
cally had the highest probability of catastrophic
failure for rocket-propelled vehicles.
Anomaly Reporting
Analyses of mishaps often show that clues
existed before the mishap in the form of anomalies
during the project life cycle. Examination and
understanding of launch vehicle system and subsys-
tem anomalies throughout the life cycle can warn of
an impending mishap and can provide important
information about what conditions need to be con-
trolled to mitigate public risk. Because of this, the
FAA has placed special emphasis on anomaly
reporting in the experimental permit regime.iv
A launch operator must record anomalies and,
after analyzing the root cause of each anomaly,
implement corrective actions for those anomalies.
This would promote informed safety decisions by a
launch operator. An operator must also report to the
FAA certain safety-critical anomalies.
Guidance Documents
The FAA has developed a number of guidance
documents to assist permit applicants. These
include the following:
• AC 437.55-1, Hazard Analysis for the
Launch or Reentry of a Reusable
Suborbital Rocket Under an Experimental
Permit (April 20, 2007)
• AC 437.73-1, Anomaly Reporting and
Corrective Action for a Reusable
Suborbital Rocket Operating Under an
Experimental Permit (April 20, 2007)
• Sample Experimental Permit Application
for a Vertical Launch and Landing
Reusable Suborbital Rocket, Version 1.1,
April 2007
• Guide to Software Safety Analysis, Version
1.0, June 2006
Summary
The FAA has attempted to craft a regulatory
regime that is conducive to developmental rocket
test flights but still protects public safety. Although
streamlined compared to a license, the experimental
permit regime places great emphasis on a hazard
analysis to identify hazards and reduce risks, oper-
ating area containment, limitations on the most haz-
ardous activities, and tracking of anomalies.
Amateur Rocket Classes
Although the term amateur rocket conjures
images of young children and their parents launch-
ing model rockets from baseball fields, in fact the
FAA definition also includes rockets of consider-
ably more weight and impulse, some capable of fly-
ing to altitudes of 7,600 meters (25,000 feet) or
higher. FAA Order 7400.2F provides the Office of
Commercial Space Transportation authority to
review rocket activities where the maximum alti-
iv An anomaly is an apparent problem or failure that affects a system, a subsystem, a process, support equipment, or facilities,
and that occurs during verification or operation.
Regulatory Developments 2008 U.S. Commercial Space Transportation Developments and Concepts
72 Federal Aviation Administration Office of Commercial Space Transportation
tude achieved is greater than 7,600 meters (25,000
feet) above ground level (AGL). Under this order,
the FAA has the responsibility to regulate
unmanned rockets to ensure the safety of aircraft
flying nearby and the safety of persons and proper-
ty on the ground.
The FAA issued the first regulations applying
to unmanned rocket operations in 1963. These regu-
lations required amateur rocket operators to provide
advance notice to the FAA, and made such launches
subject to FAA approval. Amateur rockets have
grown bigger and now fly higher and farther com-
pared to when those first regulations were pub-
lished. They now have a greater potential of creat-
ing hazards beyond their launch points. As rocket
technologies have changed, regulations have been
amended to accommodate them—first in 1988, and
later in 1994.
The most recent round of amateur rocket reg-
ulatory changes was set in motion on June 14,
2007, when the FAA published a Notice of
Proposed Rulemaking (NPRM) in the Federal
Register. This action proposed a number of changes
in FAA’s regulations for unmanned rockets aimed at
preserving the safety of amateur rocket activities,
addressing inconsistencies in the current regula-
tions, and improving the clarity of the regulations.
The public was invited to comment on the proposed
changes. As of late 2007, the FAA was considering
the public comments it received to determine how
and when it may issue a final rule.
What the FAA Proposed
Under the June 2007 NPRM, the FAA pro-
posed adding two new categories of amateur rocket
operations and amending the definitions of the
existing two categories. As such, the new category
structure would be numbered from Class 1 to Class
4. The two new categories would be Class 3 (high-
powered rockets) and Class 4 (advanced high-
power rockets). These two new categories capture
amateur rockets that require significant analyses on
the part of the FAA to determine if they can be
safely launched and what operational constraints
might be necessary to preserve public safety. The
Class 1 and Class 2 rocket categories, meanwhile,
would be slightly modified to incorporate more cur-
rent definitions of model rocket and large model
rocket, respectively. Further description of these
categories follows below.
Class 1–Model Rockets
The proposed Class 1-Model Rockets would
be defined as amateur rockets using less than 125
grams (4.4 ounces) of slow-burning propellant,
made primarily of paper, wood, or breakable plas-
tic, containing no substantial metal parts, and
weighing no more than 454 grams (16 ounces),
including the propellant. This updated definition
differs from the existing definition in two ways:
maximum propellant weight and operating limita-
tions. The maximum propellant weight would be
increased from the existing 113 grams (4 ounces) to
125 grams (4.4 ounces). Additionally, Class 1-
Model Rockets would have to be “operated in a
manner that does not create a hazard to persons,
property, or other aircraft.”
Class 2–Large Model Rockets
The proposed definition of Class 2-Large
Model Rockets would only differ from Class 1 in
terms of maximum total weight. Class 2 would con-
tinue to allow rockets weighing up to 1,500 grams
(53 ounces), including propellant, in contrast to the
454 grams (16 ounces) covered by Class 1.
Class 3–High-Power Rockets
Class 3-High-Power Rockets would be
defined as amateur rockets other than model rockets
or large model rockets that are propelled by a motor
or motors having a combined total impulse of
163,840 N-sec (36,818 lb-sec) or less. In terms of
motor class, this qualifies as a “Q motor.” The FAA
would use total impulse as the distinguishing crite-
rion for high-power rockets because total impulse is
a good measure of the size, power, and performance
of the rocket.
Rockets that would be considered Class 3
under the new definition currently operate under the
provisions for Large Model Rockets. These limita-
tions would remain unchanged, but two more limi-
tations codifying current practice would be added.
The first of the new limitations would be that a per-
son at least 18 years old must be present and in
charge of ensuring the safety of the operation. The
second new limitation would require reasonable
Regulatory Developments 2008 U.S. Commercial Space Transportation Developments and Concepts
73 Federal Aviation Administration Office of Commercial Space Transportation
precautions be available to report and control a fire.
(Although this is a current practice, it would be
codified under the proposed rulemaking.)
Class 4–Advanced High-Power Rockets
Class 4-Advanced High-Power Rockets
would include any amateur rockets that do not fall
under one of the other three classes definitions. In
general, these would be rockets with a combined
total impulse above 163,840 N-sec (36,818 lb-sec),
that is, a Q motor. However, the regulation would
be written such that other, unforeseen operations or
advancements in amateur rocket technology will be
captured as Class 4.
The risk to the public from launches of this
category is often higher due to the larger amount of
propellant or stored energy within the vehicle. This
higher risk factor requires greater scrutiny. As
such, Class 4 would capture rockets more powerful
than those typically launched at amateur high-
power rocket events.
The proposed rule does not impose any addi-
tional limitations on operating Class 4-Advanced
High-Power Rockets; however, the FAA may speci-
fy operating limitations necessary to ensure that air
traffic is not adversely affected and public safety is
not jeopardized.
Information Requirements
Information requirements define data required
by the FAA to determine if a rocket can be safely
launched. Due to the low risk posed by Class 1 –
Model Rockets, operators of this class of rocket
would continue to be exempt from information
requirements. Operators of Class 2 – Large Model
Rockets would continue to provide Air Traffic
Control with their names and addresses, the highest
anticipated altitude, the location of the launch, and
the date, time, and duration of the launch event. Air
Traffic Control would then be in a position to notify
aircraft flying nearby of the rocket launches.
Under the NPRM, the FAA has proposed to
codify reporting practices for the new categories of
Class 3 and Class 4 rockets. Rockets in these class-
es currently file for a waiver to conduct their
launches. They are then exempt from launch license
regulations. Once the FAA receives the waiver
application, they usually contact the operator for
additional information. However, under the NPRM,
all information would be gathered during the initial
waiver application. Thus both the FAA and the
operators could save time and expense.
Next Steps
The FAA is now reviewing the comments
received on the NPRM. Some of these contain sug-
gestions for changes that amateur rocket operators
and others wish to see implemented before the rule
becomes final. When and if these proposed new
amateur rocket rules become final, the FAA will
publish them in the Federal Register.
1 Google Lunar X PRIZE Competition Guidelines web-page. X PRIZE Foundation. Accessed 19 November2007. http://www.googlelunarxprize.org/lunar/competi-tion/guidelines.
2 Communication with SpaceX, 27 November 2007.
3 “Armadillo Aerospace Nearly Wins NorthropGrumman Lunar Lander Challenge.” 28 October 2007.X PRIZE Foundation press release. Accessed 19November 2007. http://www.xprize.org/llc/press-release/armadillo-aerospace-nearly-wins-northrop-grumman-lunar-lander-challenge.
4 Communication with Bigelow Aerospace, 7 December2007. Also see America’s Space Prize webpage.Bigelow Aerospace. Accessed 20 November 2007.http://www.bigelowaerospace.com/multiverse/space_prizeb.php.
5 Centennial Challenges webpage. Updated 8 November2007. NASA. Accessed 19 November 2007.http://www.ip.nasa.gov/cc/index.htm.
6 “X PRIZE Foundation Announces Competitors forNorthrop Grumman Lunar Lander Challenge.” 20 June2007. X PRIZE Foundation. Accessed 29 November2007. http://space.xprize.org/lunar-lander-challenge/assets/FINAL_Wirefly_X_PRIZE_Cup_Teams_Release_6-20-07.pdf.
7 Peter Homer was subsequently contracted by a com-mercial spacesuit developer, Orbital Outfitters, forwork on their spacesuit. See Brian Berger,“Commercial Spacesuit Tailors Hire NASA ContestWinner.” 16 November 2007. SPACE.com, Accessed18 December 2007.http://www.space.com/news/0711116-private-space-suits.html.
8 “NASA's Centennial Challenges to AdvanceTechnologies.” 28 August 2007. NASA press release07-182. Accessed 19 November 2007.http://www.nasa.gov/home/hqnews/2007/aug/HQ_07182_Space_Elevator_Games.html.
9 “Centennial Challenges Descriptions and Resources.”Updated 16 May 2007. NASA. Accessed 19 November2007. http://www.ip.nasa.gov/cc/cc_challenges.htm.
10 “FY 2008 Budget Estimates.” NASA President’s FiscalYear 2008 NASA Budget Request. CASP-43. Accessed19 November 2007. http://www.nasa.gov/about/budg-et/index.html.
11 Division B – Commerce, Justice, Science and RelatedAgencies Appropriations Act, 2008.” Text of the HouseAmendments to Senate Amendment to H.R. 2764 –State, Foreign Operations, and Related ProgramsAppropriations Act, 2008 (Consolidated AppropriationsAct, 2008). U.S. House of Representatives Committeeon Rules website. Accessed 20 December 2007.http://www.rules.house.gov/110/text/omni/jes/jesdivb.pdf. Page 113.
12 Ray, Justin. “Confident Atlas rocket team ready tolaunch again”. Spaceflight Now, 7 October 2007.http://www.spaceflightnow.com/atlas/av011/071007pre-view.html. Accessed 6 November 2007.
13 Sea Launch press release. “Sea Launch ConcludesInvestigation of Launch Failure”. 11 June 2007.http://www.sea-launch.com/news_releases/nr_070611.html. Accessed 6November 2007.
14 Communication with Sea Launch Company, 7November 2007.
15 Communication with ATK, 2 January 2008.
16 Communication with Space Systems/Loral, 27November 2007.
17 E’Prime Aerospace Corp. press release. “E'PrimeAerospace Corporation Receives Launch Site PolicyReview Approval”. 5 November, 2007.http://www.marketwire.com/mw/release.do?id=788716.Accessed 5 November 2007.
18 Communication with Lockheed Martin MichoudOperations, 13 October 2006.
19 Garvey Spacecraft Corporation. “Latest News”.http://www.garvspace.com/News.htm. Accessed 5November 2007.
20 Communication with Garvey Spacecraft Corporation, 7November 2007.
21 Communication with Microcosm, Inc., 13 November2007.
22 Schoneman, Scott et al. “Minotaur V Space LaunchVehicle for Small, Cost-Effecive Moon ExplorationMissions”. 21st Annual AIAA/USU Conference onSmall Satellites, paper SSC07-III-2, 2007.
23 AirLaunch LLC press release. “AirLaunch LLC,DARPA, and U.S. Air Force Kickoff Phase 2C”. 16July 2007.http://www.airlaunchllc.com/AirLaunch%20Press%20Release%20Kickoff%20Phase%202C%20071607%20Final.pdf. Accessed 5 November 2007.
24 Communication with AirLaunch LLC, 6 November2007.
25 Berger, Brian. “Taurus 2 Coming into Focus.” SpaceNews, September 24, 2007, p. 1.
26 Communication with Zig Aerospace, 17 October 2006.
27 Communication with Sea Launch Company, 7November 2007.
28 NASA press release. “NASA Awards Upper StageEngine Contract for Ares Rockets”. 16 July 2007.http://www.nasa.gov/home/hqnews/2007/jul/HQ_C07030_J2X_Contract.html. Accessed 5 November 2007.
74 Federal Aviation Administration Office of Commercial Space Transportation
Endnotes 2008 U.S. Commercial Space Transportation Developments and Concepts
Endnotes
29 NASA press release. “NASA Selects Ares I UpperStage Production Contractor”. 28 August 2007.http://www.nasa.gov/home/hqnews/2007/aug/HQ_C07040_Ares_1_Upper_Stage_Contract.html. Accessed 5November 2007.
30 Boeing press release. “Boeing Selected to BuildInstrument Unit Avionics for NASA's Ares I CrewLaunch Vehicle”. 12 December 2007. http://www.boe-ing.com/news/releases/2007/q4/071212d_nr.html.Accessed 21 December 2007.
31 Communication with Magellan Aerospace Corporation,9 November 2007.
32 Nammo AS press release. “NAMMO successfullylaunches Hybrid Test Rocket from Andøya”. 8 May2007.http://www.nammo.com/templates/page.aspx?id=406.Accessed 5 November 2007.
33 UP Aerospace press release. “UP Aerospace, Inc.Successfully Flies Multi-faceted Space Mission.” 2May 2007.http://www.upaerospace.com/DigitalPressKit/UP_Aerospace_Inc_Post-Launch_Press_Release.pdf. Accessed 5November 2007.
34 Communication with UP Aerospace, 7 November 2007.
35 X PRIZE Foundation. “Acuity Technologies”http://space.xprize.org/lunar-lander-challenge/team_profile_acuity.php. Accessed 20December 2007.
36 Armadillo Aerospace release. “We failed.” 30 October2007.http://www.armadilloaerospace.com/n.x/Armadillo/Home/News?news_id=350. Accessed 19 November 2007.
37 Communication with Armadillo Aerospace, 20November 2007.
38 Benson Space Company press release. “Benson SpaceImproves Design of Its Spaceship”. 25 May 2007.http://www.bensonspace.com/press_details.php?id=2.Accessed 15 November 2007.
39 International Space Fellowship. “Interorbital Talk withthe Space Fellowship about Their New $1.2 MillionSatellite Mission and Joining Forces with Vision One”.27 November 2007.http://spacefellowship.com/News/?p=3806. Accessed19 December 2007.
40 Interorbital Systems. “Neptune”. http://www.interor-bital.com/Neptune%20Page_1.htm. Accessed 19December 2007.
41 Masten Space Systems. “XA-0.1 R.I.P.” 17 December2007. http://masten-space.com/blog/?p=128. Accessed19 December 2007.
42 X PRIZE Foundation. “Micro-Space”.http://space.xprize.org/lunar-lander-challenge/team_profile_micro_space.php. Accessed 20December 2007.
43 Communication with Micro-Space, 2 January 2008.
44 X PRIZE Foundation. “Paragon Labs”.http://space.xprize.org/lunar-lander-challenge/team_profile_paragon_labs.php. Accessed 20December 2007.
45 PlanetSpace. “Orbital Space Flight”. http://www.planet-space.org/lo/osf.htm. Accessed 20 December 2007.
46 Rocketplane Global press release. “RocketplaneUnveils New Suborbital Vehicle Design”. 26 October2007.http://www.rocketplaneglobal.com/press/20071026a.html. Accessed 16 November 2007.
47 Rocketplane Kistler press release. “Rocketplane KistlerCompletes NASA-COTS Milestone Ahead ofSchedule.” 13 February 2007. http://www.rocket-planekistler.com/newsinfo/pressreleases/070213%20-%20PRESS%20RELEASE%20-%20RpK%20Meets%20NASA%20Milestone%20Ahead%20of%20Schedule%200207.pdf. Accessed 17November 2007.
48 NASA press release. “NASA to Open NewCompetition for Space Transportation Seed Money”. 18October 2007.http://www.nasa.gov/home/hqnews/2007/oct/HQ_07228_COTS_competition.html. Accessed 17 November2007.
49 Communication with Virgin Galactic, 17 December2007.
50 SpaceDev press release. “SpaceDev Signs Space ActAgreement with NASA for Development ofCommercial Access to Space.” 18 June 2007.http://www.spacedev.com/press_more_info.php?id=205.Accessed 17 November 2007.
51 SpaceDev press release. “SpaceDev and United LaunchAlliance to Explore Launching the Dream ChaserSpace Vehicle on an Atlas V Launch Vehicle.” 10 April2007.http://www.spacedev.com/press_more_info.php?id=5.Accessed 17 November 2007.
52 Space Access LLC press release. “Space Access OffersMajor Expansion of Space Tourism Beginning January2008”. 20 December 2007.http://www.individual.com/story.php?story=75237159.Accessed 20 December 2007.
53 SpaceX. Falcon 1 Launch Vehicle Payload User’sGuide, Rev. 6. April 2007.http://www.spacex.com/Falcon%201%20Payload%20Users%20Guide.pdf. Accessed 17 November 2007.
54 SpaceX. “Demo Flight 2 Flight Review Update”. 15June 2007. http://www.spacex.com/F1-DemoFlight2-Flight-Review.pdf. Accessed 17 November 2007.
55 SpaceX. “Falcon 9 Data Sheet” 6 April 2007.http://www.spacex.com/F9%20Data%20Sheet.pdf.Accessed 17 November 2007.
56 Communication with SpaceX, 27 November 2007.
Federal Aviation Administration Office of Commercial Space Transportation 75
2008 U.S. Commercial Space Transportation Developments and Concepts Endnotes
57 SpaceX press release. “SpaceX Signs Deal for FirstCommercial Geostationary Satellite Launch”. 14September 2007.http://www.spacex.com/press.php?page=29. Accessed17 November 2007.
58 SpaceX press release. “SpaceX Breaks Ground at CapeCanaveral’s Space Launch Complex 40”. 1 November2007. http://www.spacex.com/press.php?page=31.Accessed 17 November 2007.
59 SpeedUp. “News”.http://www.speedupworld.com/news.html. Accessed 20December 2007.
60 Communication with TGV Rockets, 19 November2007.
61 t/Space. “Projects: Crew Transfer Vehicle (CXV)”.http://www.transformspace.com/index.cfm?fuseac-tion=projects.view&workid=CCD3097A-96B6-175C-97F15F270F2B83AA. Accessed 20 December 2007.
62 X PRIZE Foundation. “Unresaonable Rocket”.http://space.xprize.org/lunar-lander-challenge/team_profile_unreasonable_rocket.php.Accessed 20 December 2007.
63 Doupe, Cole, et al. “Fully Reusable Access to SpaceTechnology FAST”. 13 March 2007.http://stinet.dtic.mil/cgi-bin/GetTRDoc?AD=ADA467945&Location=U2&doc=GetTRDoc.pdf. Accessed 17 November 2007.
64 Andrews Space press release. “Andrews Space to Workwith US Air Force on FAST Program”. 19 March 2007.http://www.andrews-space.com/news.php?subsec-tion=MjMw. Accessed 19 December 2007.
65 Lockheed Martin Michoud Operations. “LockheedMartin Awarded $14 Million Contract on U.S. AirForce Research Lab FAST Program.” 12 November2007.http://www.lockheedmartin.com/data/assets/ssc/michoud/PressReleases/LOCKHEEDMARTINAWARD-ED$14MILLIONCONTRACTONU.S.AIRFORCERE-SEARCHLABFASTPROGRAM11-12-07.pdf.Accessed 19 December 2007.
66 Northrop Grumman Corporation. “Northrop Grummanto Help Air Force Develop, Demonstrate Technologiesfor Reusable Launch Vehicles”. 10 December 2007.http://www.irconnect.com/noc/press/pages/news_releas-es.html?d=132818. Accessed 19 December 2007.
67 Orion Crew Vehicle webpage. Updated 5 November2007. NASA Constellation Program. Accessed 29November 2007.http://www.nasa.gov/mission_pages/constellation/orion/index.html.
68 “Constellation Program: Astronaut Safety in a LaunchEmergency. The Orion Launch Abort System.” NASAFacts. FS-2007-07-136-LaRC. Accessed 29 November2007.
69 “Constellation Program: America’s Spacecraft for aNew Generation of Explorers. The Orion CrewExploration Vehicle”. NASA Facts. FS-2006-08-022-JSC. Accessed 29 November 2007.
70 “NASA to Open New Competition for SpaceTransportation Seed Money.” 18 October 2007. NASApress release 07-228. Accessed 28 November 2007.http://www.nasa.gov/home/hqnews/2007/oct/HQ_07228_COTS_competition.html.
71 Communication with SpaceX, 27 November 2007.
72 See company press releases and information for thenew COTS Phase 1 system proposal information:
Constellation Services International: “Constellation Services International and Space Systems Loral Team On NASA COTS Proposal Using a U.S. Version of CSI’s LEO EXPRESS Cargo System.” 11 December 2007. CSI news release. Accessed 19 December 2007. http://www.constellationservices.com/Press_Release_20071211.pdf.
PlanetSpace: “PlanetSpace, Lockheed Martin and ATK team up to bid on NASA COTS.” 21 November 21, 2007. PlanetSpace press release. Accessed 19 December 2007. http://www.planetspace.org/pdf/PressRelease112107.pdf.
SpaceDev: SpaceDev Advanced Systems webpage. Accessed 19 December 2007. http://www.spacedev.com/spacedev_advanced_systems.php
SPACEHAB: “SPACEHAB Responds to NASARFP Seeking Commercial ISS Resupply Means.” 29 November 2007. SPACEHAB press release. Accessed 19 December 2007. http://www.spacehab.com/news/2007/07_11_29.htm.
t/Space: “t/Space enters COTS second round .” November 29, 2007. t/Space News and Media webpage. Accessed 19 December 2007. http://www.transformspace.com/index.cfm?fuseaction=news.view&newsid=8D34F05A-E7F7-11C1-74E37AB2DBDA99CC.
Andrews Space: “Andrews Space Reveals Cargo Vehicle Design Work.” 12 December 2007. Andrews Space press release. Accessed 19 December 2007. http://www.andrews-space.com/news.php?subsection=Mjk3.
73 Lopez, C. Todd Staff Sgt., USAF. “Unmanned vehicleprovides reusable test capabilities in space.” 17November 2006. Air Force Print News online.Accessed 28 November 2007.http://www.af.mil/news/story.asp?storyID=123032226.
76 Federal Aviation Administration Office of Commercial Space Transportation
Endnotes 2008 U.S. Commercial Space Transportation Developments and Concepts
74 Shiga, David. “Bigelow Aerospace to offer $760 mil-lion for spaceship.” 25 October 2007. New ScientistSpace online. Accessed 22 November 2007.http://space.newscientist.com/article/dn12836-bigelow-aerospace-to-offer-760-million-for-spaceship.html.
75 Communication with Bigelow Aerospace, 7 December2007.
76 Communication with Space Exploration TechnologiesCorporation, 27 November 2007.
77 Communication with Microcosm, Inc., 27 November2007.
78 Communication with ATK, Inc., 3 January 2008.
79 ATK press release. “ATK Receives $1.8 BillionContract to Develop and Support Test Flights forNASA's Ares I Crew Launch Vehicle First Stage” 13August 2007.http://atk.mediaroom.com/index.php?s=press_releas-es&item=739. Accessed 4 January 2008.
80 Communication with AirLaunch LLC, 23 November2007.
81 AirLaunch LLC press release. “AirLaunch LLC,DARPA, and U.S. Air Force Kickoff Phase 2C.”AirLaunchLLC, 16 July 2007. http://www.airlaunch-llc.com/News.htm. Accessed 13 November 2007.
82 Communication with Garvey Spacecraft Corporation,19 November 2007.83 Northrop Grumman pressrelease. “Northrop Grumman Demonstrates NewRocket Engine Design Using Oxygen and MethanePropellants.” Northrop Grumman Corporation, 14November 2007.http://www.irconnect.com/noc/press/pages/news_releas-es.html?d=131378. accessed 13 December 2007.
84 NASA Facts Sheet. “The J–2X Engine”. Doc.#FS–2007–08–111–MSFC8–328472, 2007.http://www.nasa.gov/pdf/187393main_j-2x_fact_sheet.pdf. Accessed 27 November 2007.
85 NASA press release. “NASA's J-2X Powerpack TestingStatus Report #1” NASA. 19 December 2007.http://www.nasa.gov/centers/marshall/news/news/releases/2007/07-143.html. Accessed 20 December 2007.
86 Pratt & Whitney Rocketdyne press release. “Pratt &Whitney Rocketdyne Awarded $1.2 Billion NASAContract for J-2X Ares Rocket Engine”. 18 July 2007.http://www.pw.utc.com/vgn-ext-templating/v/index.jsp?vgnextoid=2e35288d1c83c010VgnVCM1000000881000aRCRD&prid=e480c230314d3110VgnVCM100000c45a529f. Accessed 20 November2007.
87 SpaceX press release. “SpaceX CompletesDevelopment of Merlin Regeneratively Cooled RocketEngine.” SpaceX, 12 November 2007.http://home.businesswire.com/portal/site/google/index.jsp?ndmViewId=news_view&newsId=20071112005019&newsLang=en. Accessed 13 November 2007.
88 SpaceX press release. “SpaceX CompletesDevelopment of Merlin Regeneratively Cooled RocketEngine.” SpaceX, 12 November 2007.
89 SpaceX press release. “SpaceX CompletesDevelopment of Merlin Regeneratively Cooled RocketEngine.” SpaceX, 12 November 2007.http://home.businesswire.com/portal/site/google/index.jsp?ndmViewId=news_view&newsId=20071112005019&newsLang=en. Accessed 13 November 2007.
90 Communication with Space Exploration Technologies,27 November 2007.
91 SpaceX press release. “SpaceX CompletesDevelopment of Merlin Regeneratively Cooled RocketEngine.” SpaceX, 12 November 2007.http://home.businesswire.com/portal/site/google/index.jsp?ndmViewId=news_view&newsId=20071112005019&newsLang=en. Accessed 13 November 2007.
92 NASA feature. “Methane Blast.” Science@NASAwebsite, 4 May 2007.|http://science.nasa.gov/headlines/y2007/04may_methaneblast.htm. Accessed 13 November 2007.
93 Grossman, Lev. “The Best Inventions of The Year.”Time Magazine, 12 November 2007, p. 78.
94 XCOR Aerospace press release. “ATK and XCORSuccessfully Complete Test Series
for NASA's 7,500 lbf-thrust LOX/Methane WorkhorseEngine”. XCOR Aerospace. 12 December 2007.http://www.xcor.com/press-releases/2007/07-12-12_ATK_and_XCOR_complete_LOX_methane_test-ing.html. Aaccessed 18 December 2007.
95 Boyle, Alan. “Rocket Racer Revealed”. Cosmic Log. 7November 2007.http://cosmiclog.msnbc.msn.com/archive/2007/11/07/454487.aspx. Accessed 25 November 2007.
96 Orion Propulsion Inc. press release. “Latest News -October 2006.” Orion Propulsion Inc., October 2006.http://orionpropulsion.com/latestnews.php. Accessed 11October 2006.
97 Orion Proulsion Inc. press release. “Latest News:Innovative Thruster Module Successfully Tested” OrionPropulsion Inc. 7 December 2007. http://www.orion-propulsion.com/. Accessed 20 December 2007.
98 Communication with Space Exploration Technologies,27 November 2007.
99 Orbital press release. “Orbital To Provide Launch AbortSystem For NASA’s Orion Crew Exploration Vehicle”1 September 2006.http://www.orbital.com/newsinfo/release.asp?prid=570.Accessed 26 November 2007.
100 NASA press release. “NASA to Break Ground forOrion Test Pad at White Sands, N.M.” 8 November2007.http://www.nasa.gov/home/hqnews/2007/nov/HQ_M07158_ESMD_White_Sands_Groundbreaking.html.Accessed 4 January 2008.
101 Orbital fact sheet. “Orion Crew Exploration VehicleLaunch Abort System (LAS)” Orbital SciencesCorporation. 2006.http://www.orbital.com/NewsInfo/Publications/LAS_Fact.pdf#search="launch abort system. Accessed 26November 2007.
Federal Aviation Administration Office of Commercial Space Transportation 77
2008 U.S. Commercial Space Transportation Developments and Concepts Endnotes
102 Pratt & Whitney Rocketdyne press release. “Pratt &Whitney Rocketdyne’s Revolutionary Scramjet EngineSuccessfully Powers First X-51A Simulated Flight”Pratt & Whitney Rocketdyne. 30 April 2007.http://www.pw.utc.com/vgn-ext-templating/v/index.jsp?vgnextoid=2e35288d1c83c010VgnVCM1000000881000aRCRD&prid=0c8381dc89e22110VgnVCM100000c45a529f____. Accessed 13December 2007.
103 Andrews Space Inc. press release. “Andrews AwardedDARPA/AFRL Contract to Demonstrate In-FlightPropellant Generation For Advanced SpaceTransportation.” Andrews Space, Inc., 27 March 2006.http://www.andrews-space.com/news.php?subsec-tion=MjA1. Accessed 16 October 2006.
104 Communication with Andrews Space, Inc. 21December 2007.
105 Air Launch LLC press release. “Operational C-17AUsed to Break Another Record with Air Launch inDARPA/Air Force Falcon Small Launch VehicleProgram.” Air Launch LLC, 27 July 2006. www.cali-forniaspaceauthority.org/images/pdfs/pr060801-1.pdf.Accessed 10 October 2006.
106 Communication with AirLaunch LLC., 23 November2007.
107 Andrews Space press release. “Andrews SpaceDevelops Advanced Thermal Protection Materials forReentry Applications”. Andrews Space. 20 December2007. http://www.andrews-space.com/news.php?sub-section=Mjk4. Accessed 20 December 2007.
108 Boeing press release. “Boeing Completes PrototypeHeat Shield for NASA Orion Spacecraft” Boeing, 13November 2007.http://www.boeing.com/ids/news/2007/q4/071113a_nr.html. Accessed 20 November 2007.
109 NASA press release. “Success for Second Ares MainParachute Test” 15 November 2007.http://www.nasa.gov/mission_pages/constellation/multi-media/photos07-126_2.html. Accessed 20 December2007.
110 Alliant Techsystems press release. “World’s largestRocket Stage Recovery Parachute Test is Successful” 2October 2007.http://atk.mediaroom.com/index.php?s=press_releas-es&item=752. Accessed 14 November 2007.
111 “Final Environmental Assessment for the ProposedBlue Origin West Texas Launch Site.” FAA/AST,August 2006.http://www.faa.gov/about/office_org/headquarters_offices/ast/media/20060829_Blue_Origin_EA_Signed.pdf.Accessed 08 November 2006.
112 “AST Issues First Experimental Permit for a ReusableSuborbital Rocket to Blue Origin.” FAA/AST, 25September 2006.http://ast.faa.gov/Exper_Permit_Blue_Origin.htm.Accessed 8 November 2006
.113 Communication with California Spaceport, 21November 2007.
114 Ibid.
115 Communication with Space Florida, 26 November2007.
116 Ibid.
117 Ibid.
118 Ibid.
119 Ibid.
120 Ibid.
121 Communication with Mid-Atlantic Regional Spaceport,8 November 2007.
122 Ibid.
123 Ibid.
124 Ibid.
125 Communication with Mojave Airport, 17 October 2006.
126 David, Leonard. “XCOR Rocket Plane Soars intoRecord Book.” SPACE.com, 3 December 2005.http://www.space.com/missionlaunches/051203_xcor_flight.html. Accessed 28 December 2005.
127 Boyle, Alan. “Regulators OK Oklahoma Spaceport.”MSNBC, 13 June 2006.http://www.msnbc.msn.com/id/13304491. Accessed 2November 2006.
128 Ibid.
129 Communication with Oklahoma Space IndustryDevelopment Authority, 26 October 2006.
130 Ibid.
131 Communication with Cape Canaveral Air ForceStation, 30 September 2005.
132 Department of the Air Force, Edwards Air Force Base.“Memorandum for Government Agencies, PublicOfficials, Libraries, Public Groups, and InterestedIndividuals.” U.S. Air Force, December 2002.http://www.ealev.com. Accessed 7 November 2006.
133 NASA Press Release (58-06). “NASA RequestsProposals for Exploration Park Developer.” NASA, 1September 2006.http://www.nasa.gov/centers/kennedy/news/releas-es/2006/release-20060901.html. Accessed 3 November2006.
134 NASA Press Release (04-06). “GlobalFlyer AircraftArrival Set for This Week.” NASA, 9 January 2006.http://www.nasa.gov/centers/kennedy/news/releas-es/2006/release-20060109.html. Accessed 3 November2006.
135 NASA Press Release (06-132). “NASA and ZERO-GAgree on Regular Shuttle Runway Use.” NASA, 4April 2006.http://www.nasa.gov/centers/kennedy/news/releas-es/2006/release-20060404.html. Accessed 3 November2006.
78 Federal Aviation Administration Office of Commercial Space Transportation
Endnotes 2008 U.S. Commercial Space Transportation Developments and Concepts
136 NASA RFI-SLF-1. “Request For InformationSupporting an Environmental Assessment ofCommercial and other uses of the Shuttle LandingFacility.” NASA, 29 September 2006. http://procure-ment.nasa.gov/cgi-bin/eps/sol.cgi?acqid=122399#Other%2001, Accessed3 November 2006.
137 “KSC Hosts Private Jet's Suborbital PathfinderFlights.” 12 April 2007.http://www.vmaxmarketing.com/news/nasa1.htm.Accessed 3 January 2008.
138 Communication with Reagan Test Site, 6 November2007.
139 Communication with Reagan Test Site, 20 October2006.
140 Communication with Vandenberg Air Force Base, 7October 2005.
141 Communication with NASA Wallops Flight Facility, 11October 2005.
142 Communication with Wallops Flight Facility, 15November 2007.
143 Ibid.
144 Communication with White Sands Missile Range, 6October 2005.
145 Communication with White Sands Missile Range, 1December 2007.
146 Communication with Cecil Field Spaceport, 20November 2007.
147 Ibid.
148 Communication with Chugwater Spaceport, 14December 2007.
149 Communication with Aerospace Development Center,23 September 2004.
150 Reid, T.R. “N.M. Plans Launchpad for Space Tourism.”The Washington Post, 15 December 2005.http://www.washingtonpost.com/wp-dyn/content/arti-cle/2005/12/14/AR2005121402340.html. Accessed 3November 2006.
151 Communication with Office for SpaceCommercialization, New Mexico EconomicDevelopment Department, 21 November 2007.
152 Ibid.
153 “Pact Clears the Way for New Spaceport Site. NewMexico Signs Agreement on Access to 15,000 acres ofState Trust Land.” Associated Press, 11 January 2006.http://msnbc.msn.com/id/10807954. Accessed 3November 2006.
154 David, Leonard. “New Mexico Inks Spaceport FundingPackage.” SPACE.com, 2 March 2006.http://www.space.com/news/060302_newmexico_update.html. Accessed 3 November 2006.
155 Communication with Office for SpaceCommercialization, New Mexico EconomicDevelopment Department, 21 November 2007.
156 Ibid.
157 Communication with Space Explorers, 21 November2007.
158 2005 Senate Bill 352. Wisconsin State Legislature, 28September 2005.http://www.legis.state.wi.us/2005/data/SB-352.pdf.Accessed 21 November 2006.
159 Egan, Dan. “With All Systems Go, Sheboygan Shootsfor the Moon with Spaceport.” The Milwaukee JournalSentinel, 12 May 2006.http://www.findarticles.com/p/articles/mi_qn4196/is_20060512/ai_n16370976/print. Accessed 7 November2006.
160 Communication with Space Explorers, 21 November2007.
161 Communication with Port of Moses Lake, 6 October2006.
162 Communication with Spaceport Washington, 27September 2005.
163 Communication with Port of Moses Lake, 6 October2006.
164 Pecos County Aerospace Development CenterTechnical Description. Pecos County West Texas“Westex” Spaceport Development Corporation, 2006.http://www.aerospacetexas.com/uguide/index.html.Accessed 21 November 2006.
165 Communication with Pecos County West Texas“Westex” Spaceport Development Corporation, 10October 2005.
2008 U.S. Commercial Space Transportation Developments and Concepts Endnotes
Federal Aviation Administration Office of Commercial Space Transportation 79
Page 6
Lunar rover mockup at launch of Google Lunar XPRIZE, courtesy of the X PRIZE Foundation
Page 7
Flight of Armadillo Aerospace’s MOD-1 vehicle for the2007 Northrup Grumman Lunar Lander Challenge,courtesy of Armadillo Aerospace
Page 9
Atlas V, courtesy of United Launch Alliance
Delta II, courtesy of United Launch Alliance
Page 10
Delta IV Heavy, courtesy of United Launch Alliance
Page 11
Minotaur, courtesy of Orbital Sciences Corporation
Pegasus XL, courtesy of Orbital Sciences Corporation
Taurus, courtesy of Orbital Sciences Corporation
Page 12
Zenit-3SL, courtesy of Sea Launch Company, LLC
ALV, courtesy of Alliant Techsystems
Page 13
Aquarius vehicle illustration, courtesy of SpaceSystems/Loral
Aquarius mission profile, courtesy of SpaceSystems/Loral
Eaglet and Eagle, courtesy of E’Prime AerospaceCorporation
Page 14
FALCON SLV, courtesy of Lockheed MartinCorporation
Prospector 8A, courtesy Joe Mullen/Garvey SpacecraftCorporation
Page 15
Sprite SLV, courtesy of Microcosm, Inc.
Minotaur IV, courtesy of Orbital Sciences Corporation
Page 16
QuickReach, courtesy of AirLaunch, LLC
Page 17
Zenit-3SLB, courtesy of Sea Launch Company, LLC
Ares I, courtesy of NASA
Ares V, courtesy of NASA
Page 18
Black Brant, courtesy of Bristol Aerospace Limited
Page 19
Oriole, courtesy of DTI Associates
Terrier-Orion, courtesy of DTI Associates
Page 20
SpaceLoft XL, courtesy of UP Aerospace
Page 21
Tiger and Cardinal, courtesy of Acuity Technologies
Page 22
MOD-1, courtesy of Armadillo Aerospace
BSC Spaceship, courtesy of Benson Space Company
Blue Origin’s Goddard prototype vehicle, courtesy ofBlue Origin
Page 23
Sea Star, courtesy of Interorbital Systems
Neptune, courtesy of Interorbital Systems
Page 24
XA 1.0, courtesy of Masten Space Systems
Crusader LL, courtesy of Micro-Space
Page 25
Volkon, courtesy of Paragon Labs
Silver Dart, courtesy of PlanetSpace
Page 26
Rocketplane XP, courtesy of Rocketplane Global
K-1, courtesy of Rocketplane Kistler
Page 27
SpaceShipTwo, courtesy of Virgin Galactic
Dream Chaser, courtesy of SpaceDev
Page 28
Skyhopper, courtesy of Space Access LLC
Falcon 1, courtesy of Space Exploration TechnologiesCorporation
Page 29
Falcon 9, courtesy of Space Exploration TechnologiesCorporation
Laramie Rose, courtesy of SpeedUp
Page 30
Michelle-B, courtesy of TGV Rockets, Inc
Crew Transfer Vehicle, courtesy of t/Space
Burning Splinter, courtesy of of Unreasonable Rocket
80 Federal Aviation Administration Office of Commercial Space Transportation
2008 U.S. Commercial Space Transportation Developments and Concepts Photo Credits
Photo Credits
Page 31
Xerus, courtesy of XCOR Aerospace, Inc.
Space Shuttle, courtesy of NASA
Page 33
Orion CEV, courtesy of Lockheed Martin Corporation
Page 34
SpaceX Dragon, courtesy of Space ExplorationTechnologies Corporation
Page 35
SpaceX Dragon crew concept, courtesy of SpaceExploration Technologies Corporation
X-37 concept, courtesy of NASA
Page 36
External view of Genesis II with the Earth in the back-ground, courtesy of Bigelow Aerospace
Page 37
Bigelow module concept, courtesy of BigelowAerospace
Page 38
Falcon 9 first stage, courtesy of Space ExplorationTechnologies Corporation
Microcosm composite tanks, courtesy of Microcosm,Inc.
Page 39
Five-segment motor test, courtesy of AlliantTechsystems
AirLaunch hot fire test, courtesy of AirLaunch LLC
Page 40
P-8A static fire test, courtesy of Garvey SpacecraftCorporation
Page 41
J-2 test, courtesy of NASA
Merlin 1C test firing, courtesy of Space ExplorationTechnologies Corporation
Page 42
XCOR XR-5M15 test fire, courtesy of XCORAerospace, Inc.
Orion thruster test, courtesy of Orion Propulsion, Inc.
Page 43
Draco thruster, courtesy of Space ExplorationTechnologies Corporation
Conceptual Orion launch abort system, courtesy ofOrbital Sciences Corporation
X-1 scramjet test, courtesy of Pratt & WhitneyRocketdyne, Inc.
Page 44
Andrews ACES test, courtesy of Andrews Space, Inc.
QuickReach Drop Test, courtesy of AirLaunch LLC
Page 45
Prototype heat shield, courtesy of The BoeingCompany
Parachute testing at Yuma Proving Ground, courtesy ofNASA
Page 49
California Spaceport SLC-8, courtesy of CaliforniaSpaceport
Space Florida SLC-46 MAS, courtesy of Space Florida
Page 50
FTG-03 Launch from Kodiak Launch Complex, cour-tesy of the U.S. Missile Defense Agency
Page 51
NFIRE launch from Mid-Atlantic Regional Spaceport,courtesy of Mid-Atlantic Regional Spaceport
Page 53
Mojave Air and Space Port, courtesy of Mojave Air andSpace Port
Page 54
Oklahoma Spaceport, courtesy of Oklahoma SpaceIndustry Development Authority
Page 55
Cape Canaveral Air Force Station, courtesy of U.S. AirForce/Master Sgt. Jack Braden
Page 57
Shuttle landing at Edwards Air Force Base, courtesy ofEdwards Air Force Base
Lauch of Space Shuttle Discovery mission STS 114,courtesy of NASA
Page 58
Interceptor launched from Meck2 at Reagan Test Site,courtesy of Reagan Test Site
Delta II preparing for launch, courtesy of VandenbergAir Force Base
Page 59
Wallops Flight Facility, courtesy of Wallops FlightFacility
Page 60
White Sands Missile Range, courtesy of White SandsMissile Range
Page 62
Cecil Field aerial view, courtesy of Cecil FieldSpaceport
Federal Aviation Administration Office of Commercial Space Transportation 81
Photo Credits 2008 U.S. Commercial Space Transportation Developments and Concepts
Page 63
Chugwater aerial view, courtesy of ChugwaterSpaceport
Page 64
Cutaway view of Spaceport America facility, courtesyof Spaceport America
Page 65
Rocket launch from Spaceport Sheboygan, courtesy ofRockets for Schools
Page 66
Spaceport Washington aerial view, courtesy ofSpaceport Washington
Photo Credits 2008 U.S. Commercial Space Transportation Developments and Concepts
82 Federal Aviation Administration Office of Commercial Space Transportation